Multidisciplinary aerospace design optimization: Survey of recent developments

Structural Optimization

Volumn 14, Issue 1, 1997, Pages 1-23

  Sobieszczanski Sobieski, J ^a   Haftka, R T ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; APPROXIMATION THEORY; MATHEMATICAL MODELS; OPTIMIZATION; SENSITIVITY ANALYSIS; USER INTERFACES;

MULTIDISCIPLINARY OPTIMIZATION (MDO);

STRUCTURAL DESIGN;

EID: 0031211068     PISSN: 09344373     EISSN: None     Source Type: Journal    
DOI: 10.1007/BF01197554     Document Type: Article

References (356)

1. Abdi, F.F.; Ide, H.; Shankar, V.M.; Sobieszczanski-Sobieski, J. 1988: Optimization for non-linear aeroelastic tailoring criteria. 16th Cong. Int. Council for Aeronaut. Sci., pp. 1083-1091. Washington, D.C.: AIAA
2. Adelman, H. M.; Haftka, R.T. 1993: Sensitivity analysis of discrete systems. In: Kamat, M.P. (ed.) Structural optimization: status and promise. Washington, D.C.: AIAA
3. Adelman, H.M.; Mantay, W.R. 1991: Integrated multidisciplinary design optimization of rotorcraft. J. Aircraft 28, 22-28
4. Adelman, H.; Walsh, J.; Pritchard, J. 1992: Recent advances in integrated multidisciplinary optimization of rotorcraft. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92 -4777
5. American Institute of Aeronautics and Astronautics, Inc. (AIAA) 1991: Current state of the art of multidisciplinary design optimization. Prepared by the AIAA Technical Committee for MDO and approved by AIAA Technical Activities Committee, Washington, D.C.
6. Alexandrov, N. 1993: Multilevel algorithm for nonlinear equations and equality constrained optimization. Ph.D. Dissertation, Dept. of Computational and Applied Mathematics, Rice University, Houston, TX
7. Alexandrov, N. 1996: Robustness properties of a trust region Framework for managing approximations in engineering optimization. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 1056-1059. AIAA Paper No. 96-4102
8. Alexandrov, N; Dennis, J.E., Jr. 1994a: Multilevel algorithms for nonlinear optimization. In: Burkardt, J.; Gunzburger, M.; Peterson, J. (eds.) Optimal design and control. Borggaard
9. Alexandrov, N; Dennis, J.E., Jr. 1994b: Algorithms for bilevel optimization. Proc. AIAA/NASA/USAF/ISSMO 5th Symp. on Multidisciplinary Analysis and Optimization (held in Panama City, FL). AIAA CP-91-4334
10. Alexandrov, N.; Hussaini, M.Y. (eds.) 1995: Multidisciplinary design optimization: state of the art. Proc. Workshop organized by the Institute for Computer Applications in Science and Engineering (ICASE) (held at NASA Langley Research Center, Hamp ton, VA)
11. Altus, S.; Bischof, C.; Hovland, P.; Kroo, I. 1996: Using automatic differentiation with the quasi-procedural method for multidisciplinary design optimization. Presented at the 34th AIAA Aerospace Sciences Conf. (held in Reno, Nevada)
12. Altus, S.; Kroo, I.; Gage, P. 1995: A genetic algorithm for scheduling and decomposition of multidisciplinary design problems. Proc. ASME Design Automation Conf. (held in Boston, MA)
13. Arora, J.; Lin, T.: 1992 A study of augmented Larangian methods for simultaneous optimization of controls and structures. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 9 2-4789
14. Arslan, A.E.; Carlson, L.A. 1996: Integrated determination of sensitivity derivatives for an aeroelastic transonic wing. J. Aircraft 33, 224-231
15. August, R.; Yamamoto, O.; Shimko, R. 1992: Integrated structural-aerodynamic analyzer. Proc. 4th AIAA/NASA/USAF/OAI Symp. Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4699
16. Baker M.; Giesing, J. 1995: A practical approach to MDO and its application to an HSCT aircraft. 1st AIAA Aircraft Engineering, Technology, and Operations Cong. (held in Los Angeles, CA). AIAA Paper No. 95-3885
17. Balabanov, V.; Kaufman, M.; Giunta, A.A.; Haftka, R.T.; Grossman, B.; Mason, W.H.; Watson, L.T. 1996: Developing customized wing weight function by structural optimization on parallel computers. Proc. 37th AIAA/ASME/ASCE/AHS Structures, Structura l Dynamics, and Materials Conf.: Part 1 (held in Salt Lake City, UT). AIAA Paper 96- 1336, pp. 113-125
18. Balling, R.J.; Sobieszczanski-Sobieski, J. 1995: An algorithm for solving the system- level problem in multilevel optimization. Struct. Optim. 9, 168-177
19. Balling, R.J.; Sobieszczanski-Sobieski, J. 1994: Optimization of coupled systems: a critical overview. AIAA/NASA/USAF/ISSMO 5th Symp. on Multidisciplinary Analysis and Optimization (held in Panama City, FL). AIAA Paper No. 94-4330 (Publication in AIAA J. pending)
20. Balling, R., Wilkinson, C. 1996: Execution of multidisciplinary design optimization approaches on common test Ppoblems. it Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4033
21. Barthelemy, J.-F.M.; Hall, L.E. 1995: Automatic differentiation as a tool in engineering design. Struct. Optim. 9, 76-82
22. Barthelemy, J.-F; Sobieszczanski-Sobieski, J. 1983: Optimum sensitivity derivatives of objective functions in nonlinear programming. AIAA J. 21, 913-915
23. Barthelemy, J.-F.M.; Haftka, R.T. 1993: Approximation concepts for optimum structural design - A review. Struct. Optim. 5, 129-144
24. Barthelemy, J.-F.; Wrenn, G.; Dovi, A.; Coen, P. 1992: Integrating aerodynamics and structures in the minimum weight design of a supersonic transport wing. Presented at AIAA/ASME/ASCE/AHS/ASC 33rd Structures, Structural Dynamics, and Materials Conf. (held in Dallas, TX). AIAA Paper No. 92-2372
25. Bartholomew, P.; Wellen, H.K. 1990: Computer-aided optimization of aircraft structures. J. Aircraft 27, 1079-1086
26. Bearden, D.; Coleman, G.; Streeter, T. 1994: An end-to-end simulation to support optimization of a multi-function space-based surveillance system. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panam a City, FL). AIAA Paper No. 94-4371
27. Beltracchi, T.J. 1990: A decomposition approach to solving the trajectory optimization problem. Proc. AIAA Aerospace Sciences Meeting (held in Reno, Nevada). AIAA Paper 90-0469. Also: AIAA J. Guidance Control and Dynamics, 1991
28. Beltracchi, T.J. 1990: A decomposition approach to solving the trajectory optimization problem. Proc. AIAA Aerospace Sciences Meeting (held in Reno, Nevada). AIAA Paper 90-0469. Also: AIAA J. Guidance Control and Dynamics, 1991
29. Berkes, U.L. 1990: Efficient optimization of aircraft structures with a large number of design variables. J. Aircraft 27, 1073-1078
30. Bil, C. 1988: Development and application of a computer based system for conceptual aircraft design. Delft: Delft University Press
31. Bindolino, G.; Lanz, M.; Mantegazza, P.; Ricci, S. 1990: Integrated structural optimization in the preliminary aircraft design. Proc. 17th Cong. Int. Council of the Aeronautical Sciences (held in Stockholm), pp. 1366-1378
32. Bischof, C.; Knauff, T., Jr. 1994: Parallel calculation of sensitivity derivatives for aircraft design using automatic differentiation. 5th AIAA/USAF/NASA/ISSMO Symp. Multidisciplinary Analysis and Optimization (held in Panama City, FL). AIAA Paper No. 2E 94-4261
33. Bloebaum, C.L.; Hajela, P.; Sobieszczanski-Sobieski, J. 1992: Non-hierarchic system decomposition in structural optimization. Eng. Opt. 19, 171-186
34. Bloebaum, C.L. 1991: Formal and heuristic system decomposition in structural optimization. NASA CR-4413
35. Bloebaum, C.L. 1992: An intelligent decomposition approach for coupled engineering systems. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No.92-4821
36. Bloebaum, C.L. 1996: Coupling strength-based system reduction for complex engineering design. Struct. Optim. (to be published)
37. Bloebaum, C.L.; Hajela, P.; Sobieski, J. 1993: Decomposition methods for multidisciplinary synthesis. Multidisciplinary engineering systems: design and optimization techniques and their application. In: Leondes, C.T. (ed.) Controls and dynamic systems 57, pp. 1-24. New York: Academic Press
38. Bodden, D.S.; Junkins, J.L. 1985: Eigenvalue optimization algorithms for structure/controller design iterations. J. Guidance, Control, and Dynamics 8, 697-706
39. Bohnhoff, A.; Brandt, D.; Henlling, K. 1992: Design as a tool for the interdisciplinary design of human-centered systems. Int. J. Human Factors in Manufacturing 2, 289-301
40. Borland, C.J.; Benton, J.R.; Frank, P.D.; Kao, T.J.; Mastro, R. A.; Barthelemy, J.-F.M. 1994: Multidisciplinary design optimization of a commercial aircraft wing - An exploratory study. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. Multidisciplinary Analysis and Optimization (held in Panama City, FL). AIAA Paper 94-4305-CP, Vol. 1, pp. 505-519
41. Brama, T.; Rosengren, R. 1990: Applications of structural optimization software in the design process. J. Aircraft 27, 1057-1059
42. Braun, R.D. 1996: Collaborative optimization: an architecture for large-scale distributed design. Ph.D. Dissertation, Department of Aeronautics and Astronautics, Stanford University, Stanford, CA
43. Braun, R.D.; Kroo, I.M. 1996: Development and application of the collaborative optimization architecture in a multidisciplinary design environment. In: Alexandrov, N., Hussaini, M.Y. (eds.) Multidisciplinary design optimization: state of the art. SIAM J. Optimization
44. Braun, R.D.; Kroo, I.M.; Gage, P.Y. 1993: Post-optimality analysis in aircraft design. Proc. AIAA Aircraft, Design, Systems, and Operations Meeting (held in Monterey, CA). AIAA Paper No. 93-3932
45. Braun, R.D.; Powell, R.W.; Lepsch, R.A.; Stanley, D.L.; Kroo, I.M. 1995: Comparison of two multidisciplinary optimization strategies for launch vehicle design. J. Spacecraft and Rockets 32, 404-410
46. Braun, R.; Moore, A.; Kroo. I, 1996: Use of the collaborative optimization architecture for launch vehicle design. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4082
47. Brewer, J.; Donofrio, K.; Mavris, D.; Schrage, D. 1994: Implementation of Georgia Tech's concurrent engineering methodology to a high speed civil transport. AIAA/NASA/USAF/ISSMO 5th Symp. on Multidisciplinary Analysis and Optimization (held in Panama City, FL). AIAA Paper No. 94-4328
48. Briggs, H.C.; Redding, D.C.; Ih, C-H.C. 1990: Integrated control/structures/optics dynamic performance modeling of a segmented reflector telescope. ISA Paper No. 901230. In: Modeling and Simulation 21, Part 5, pp. 2077-2086.
49. Briggs, H. 1992: An Integrated modeling and design tool for advanced optical spacecraft. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4701, pp. 1153-1163
50. Brockman, J.B.; Anderson, M.; Director S.W. 1992: Efficient management of fabrication process and integrated circuit optimization tasks. Proc. IEEE Asia-Pacific Conf. on Circuit and Systems.
51. Burgee, S.; Giunta, A.A.; Narducci, R.; Watson, L.T., Grossman, B.; Haftka, R.T. 1996: A coarse grained parallel variable-complexity multidisciplinary optimization paradigm. Int. J. Supercomputer Appl. & High Performance Computing 10, 269-299
52. Callallan, C.B.; Straub, F.K. 1991: Design optimization of rotor blades for improved performance and vibration. Proc. 17th Annual Forum of the American Helicopter Society 2, 869-882
53. Canfield, R.A. 1990: High-quality approximation of eigenvalues in structural optimization. AIAA J. 28, 1116-1122
54. Celi, R. 1991: Optimum aeroelastic design of helicopter rotors for longitudinal handling qualities improvement. J. Aircraft 28, 49-57
55. Chang, K.J.; Haftka, R.T.; Giles, G.L.; Kao, P.-J. 1993: Sensitivity-based scaling for approximating structural response. J. Aircraft 30, 283-287
56. Chattopadhyay, A.; McCarty, T.R.; Pagaldipti, N. 1995: Multilevel decomposition procedure for efficient design optimization of helicopter rotor blades. AIAA J. 33
57. Chattopadhyay, A.; Pagaldipti, N. 1995: A multidisciplinary optimization using semi- analytical sensitivity analysis procedure and multilevel decomposition. J. Computers & Math. with Appl. 29, 55-66
58. Chattopadhyay, A.; Seeley, C.E. 1995: A coupled controls/structures optimization procedure for the design of rotating composite beams with piezoelectric actuators. Smart Materials & Struct. 4, 170-178
59. Chattopadhyay, A.; Walsh, J.L.; Riley, M.F. 1991: Integrated aerodynamic load/dynamic optimization of helicopter rotor blades. J. Aircraft 28, 58-65
60. Chen, W.; Allen, J.K.; Mistree, F. 1994: Robust concurrent concept selection and system synthesis. In: Gilmore, B.J.; Hoeltzel, D.; Dutta, D.; Eschenauer, H. (eds.) Advances in Design Automation, ASME DE-Vol. 69-1, pp. 141-149. New York
61. Chen, W.; Allen, J.K.; Mistree, F.; Tsui, K.-L. 1995: Integration of response surface method with the compromise DSP in developing a general robust design procedure. In: Azarm, S.; Dutta, D.; Eschenauer, H.; Gilmore, B.J.; McCarthy, J.; Yoshimura, M. (eds.) Advances in Design Automation, ASME DE-Vol. 82-2, pp. 485-492. New York
62. Claus, R.E.; Evans, A.L.; Follen, G.J. 1992: Multidisciplinary propulsion simulation using NPSS. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA-92-4709-CP, Part 1, pp. 53-62
63. Coen, P.G.; Sobieszczanski-Sobieski, J.; Dollyhigh, S.M. 1992: Preliminary results from the high-speed airframe integration research project. Aerospace Design Conf. (held in Irvine, CA). AIAA Paper No. 92-1104
64. Coen, P.; Barthelemy, J.-F.; Wrenn, G. 1992: Integration of aerodynamics and performance in the preliminary design of a supersonic transport. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, O H). AIAA Paper No.92-4718
65. Consoli, R.D.; Sobieszczanski-Sobieski, J. 1992: Application of advanced multidisciplinary analysis and optimization methods to vehicle design synthesis. J. Aircraft 29, 811-818
66. Cramer, E.J.; Dennis, J.E., Jr.; Frank, P.D.; Lewis, R.M.; Shubin, G.R. 1994: Problem formulation for multidisciplinary optimization. SIAM J. Optimiz. 4, 754-776
67. Cramer, E.J.; Huffman, W.L.; Mastro, R.A. 1993: Sparse optimization for aircraft design. AIAA Paper No. 93-3935
68. Crane, S.P.; Cunefare, K.A.; Englestad, S.P.; Powell, E. 1996: A comparison of optimization formulations for design minimization of aircraft interior noise. Proc. 37th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conf.: Part 3 (held in Salt Lake City, UT). AIAA Paper No. 96-1480, pp. 1504-1514
69. Cummings, R.M.; Freeman, H.J.A. 1996: Integrating multidisciplinary design in an undergraduate curriculum. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 807-812. AIAA Paper No. 96-4065
70. Current, J.; Min, H.; Schilling, D. 1990: Multiobjective analysis of facility location decisions. European J. Operational Research, pp. 295-307, November/December
71. Dennis, J.E., Jr.; Torczon, V. 1991: Direct search methods on parallel machines. SIAM J. Optimiz. 1, 448-474
72. Dennis, J.E.; Torczon, V. 1996: Approximation model management for optimization. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 1044-1046. AIAA Paper No. 96-4099
73. Dodd, A.J.; Kadrinka, K.E.; Loikkanen, M.J.; Rommel, B.A.; Sikes, G.D.; Strong, R.C.; Tzong, T.J. 1990: Aeroelastic design optimization program. J. Aircraft 27, 1028-1036
74. Dolvin, D. 1992: Structural design for survivability: multidisciplinary optimization employing physical linking. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4729
75. Dovi, A.R.; Wrenn, G.A. 1990: Aircraft design for mission performance using nonlinear multiobjective optimization methods. J. Aircraft 27, 1043-1049
76. Dovi, A.; Wrenn, G.; Barthelemy, J.-F.; Coen, P. 1992: Design integration for a supersonic transport aircraft. Proc. 4th AIAA/NASA/USAF/OAI Symp. Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4841
77. Dudley, J.M.; Huang, X.; Haftka, R.T.; Grossman, B.; Mason, W. H. 1994: Variable complexity interlacing of weight equations and structural optimization for the design of the high speed civil transport. Proc. 5th AIAA Multidisciplinary Analysis and Optimization Symp. (held in Panama City, FL). AIAA 94-4377-CP, pp. 1129-1134
78. Eason, E.; Merton, A. 1996: Non-hierarchic multidisciplinary design of an automobile suspension. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4082
79. Eason, E.; Wright, J. 1992: Implementation of non-hierarchic decomposition for multidisciplinary system optimization. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4 822
80. Eason, E.; Nystrom, G.; Burlingham, A.; Nelson, E. 1994a: Nonhierarchic multidisiciplinary optimal design of a commercial aircraft. AIAA/NASA/USAF/ISSMO 5th Symposium on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA-94-4302
81. Eason, E.; Nystrom, G.; Burlingham, A.; Nelson, E. 1994b: Robustness testing of nonhierarchic multidisiciplinary system optimization. AIAA/NASA/USAF/ISSMO 5th Symposium on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA-94-4302
82. General Electric Corp. 1994: A collection of papers on engineous. The Engineous Project, General Electric Corporate Research and Development, P.O. Box 8, Schenectady, NY 12301
83. Eppinger, S.D.; Whitney, D.E.; Smith, R.P.; Gebala, D.A. 1994: Model-based method for organizing tasks in product development. Research in Eng. Design G, 1-13. London: Springer
84. Fadel, G.; Bridgwood, M.; Figliola, R.; Greenstein, J.; Kostreva, M.; Nowaczyk, R.; Stevenson, D.E. 1996: Undergraduate MDA curriculum at Clemson University. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 813-818. AIAA Paper No. 96-4066
85. Fenyes, P. 1992: Structural optimization with manufacturing considerations. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4767
86. Fleury, C.; Schmit, L.A., Jr. 1980: Dual methods and approximation concepts in structural synthesis. NASA CR-3226
87. Flowers, G.; Venkayya, V. 1992: Adaptive decentralized control of flexible multibody structures. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4741
88. Forster, E.; Kolonay, R.; Venkayya, V.; Eastep, E. 1996: Optimization of a generic fighter wing incorporating active aeroelastic wing technology. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 247-257. AIAA Paper No. 96-4010
89. Frank, P.; Booker, A.; Caudell, T.; Healy, M. 1992: A comparison of optimization and search methods for multidisciplinary design. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4827
90. Friedmann, P.P. 1991: Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey. J. Aircraft 28, 8-21
91. Friedmann, P.P. 1992: Impact of structural optimization with aeroelastic/multidisciplinary constraints on helicopter rotor design. Aerospace Design Conf. (held in Irvine, CA). AIAA Paper No. 92-1001
92. Furuya, H.; Haftka, R.T. 1993: Genetic algorithms for placing actuators on space structures. Proc. Fifth Int. Conf. on Genetic Algorithms (held in Urbana, IL), pp. 536-542. Morgan Kauffman
93. Furuya, H.; Haftka, R.T. 1996: Combining genetic and deterministic algorithms for locating actuators on space structures. J. Spacecraft and Rockets 33, 422-427
94. Gage, P. 1995: New approaches to optimization in aerospace conceptual design. NASA CR-196695
95. Gage, P.; Kroo, I. 1992: Development of the quasi-procedural method for use in aircraft configuration optimization. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No.92-4693
96. Gage, P.; Kroo, I. 1995: Representation issues for design topological optimization by genetic methods. Proc. 8th Int. Conf. on Industrial and Engineering Applications of Artificial Intelligence and Expert Systems (held in Melbourne, Australia), pp. 383-388
97. Gage, P.; Braun, R.; Kroo, I. 1995: Interplanetary trajectory optimization using a genetic algorithm. J. Astronautical Sci. 43, 59-75
98. Gage, P.; Sobieski, I.; Kroo, I. 1995: A variable-complexity genetic algorithm for topological design. AIAA J. 11, 2212-2218
99. Gallman, J.W.; Kaul, R.W.; Chaildrasekharan, R.M.; Hinson, M.L. 1994: Optimization of an advanced business jet. Proc. 5th AIAA Multidisciplinary Analysis and Optimization Symp. (held in Panama City, FL). AIAA 94-4303-CP, pp. 482-492
100. Gallman, J.W.; Smith, S.C.; Kroo, I.M. 1993: Optimization of joined-wing aircraft. J. of Aircraft 30, 897-905
101. Gates, M.; Lewis, M. 1992: Optimization of spacecraft orbit and shielding for radiation dose. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4771
102. Giesing, J.P.; Agrawal, S.; Bhardvaj, B.K. 1995: The role of computational fluid dynamics in multidisciplinary design optimization of transport aircraft. Sixth Int. Symp. on Computational Fluid Dynamics (held in Lake Tahoe, CA)
103. Giles, G.L.; McCullers, L.A. 1975: Simultaneous calculation of aircraft design loads and structural member sizes. AIAA 1975 Aircraft Systems and Technology Meeting (held in Los Angeles, CA). AIAA Paper No. 75-965
104. Giunta, A.A.; Balabanov, V.; Burgee, S.; Grossman, B.; Haftka, R.T.; Mason, W.H.; Watson, L.-T. 1995: Variable-complexity multidisciplinary design optimization using parallel computers. Proc. ICES '95, Int. Conf. on Computational Engineering Science
105. Giunta, A.A.; Dudley, J.M.; Narducci, R.; Grossman, B.; Haftka, R.T.; Mason, W.H.; Watson, L.T. 1994: Noisy aerodynamic response and smooth approximations in HSCT design. Proc. 5th AIAA Multidisciplinary Analysis and Optimization Symp. (held in Panama City, FL), AIAA Paper No. 94-4376, pp. 1117-1128
106. Godse, M.; Haug, E.; Choi, K. 1992: A parametric design approach for concurrent product development. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4760
107. Grandhi, R.; Bharatram, R.; Venkayya, V. 1992: Efficient multiobjective optimization scheme for large scale structures. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4772
108. Grose, D. 1994: Reengineering the aircraft design process. AIAA/NASA/USAF/ISSMO 5th Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4323
109. Grossman, B.; Haftka, R.T.; Kao, P.-J.; Polen, D.; Rais-Rohani, M.; Sobieszczanski- Sobieski, J. 1990: Integrated aerodynamic - structural design of a transport wing. J. of Aircraft 27, 1050-1056
110. Grossman, B.; Strauch, G.; Eppard, W.H.; Gürdal, Z.; Haftka, R.T. 1988: Integrated aerodynamic/structural design of a sailplane wing. J. of Aircraft 25, 855-860
111. Gupta, S.; Joshi, S.M. 1990: An integrated control/structure design method using multi- objective optimization. NASA Workshop On Computational Control of Flexible Aerospace Systems, NASA CR-10065, Part 1, pp. 231-252
112. Haftka, R.T. 1977: Optimization of flexible wing structures subject to strength and induced drag constraints. AIAA J. 14, 1101-1106
113. Haftka, R.T. 1986: Structural optimization with aeroelastic constraints - A survey of U.S. applications. Int. J. Vehicle Design 7, 381-392
114. Haftka, R.T. 1990: Integrated structure-control optimization of space structures. AIAA/ASME/ASCE/AHS 30th Structures, Structural Dynamics, and Materials Conf. (held in Long Beach, CA). AIAA Paper 90-1190
115. Haftka, R.T.; Adelman, H. 1989: Recent developments in structural sensitivity analysis. Struct. Optim. 1, 137-151
116. Haftka, R.T.; Gürdal, Z. 1992: Elements of structural optimization, 3rd edition. Dordrecht: Kluwer
117. Haftka, R.T.; Grossman, B.; Eppard, W.M.; Kao, P.J.; Polen, D. 1989: Efficient optimization of integrated aerodynamic-structural design. Int. J. Num. Meth. Engrg. 28, 593-607
118. Haftka, R.T.; Balabanov, V.; Burgee, S.; Giunta, A.; Grossman, B.; Kaufman, M.; Mason, W.H.; Watson, L.T. 1995: Variable-complexity aerodynamic-structural optimization via response surface techniques. Proc. ICASE/LaRC Workshop on Multidisciplinary Design Optimization (held in Hampton, VA) (to appear)
119. Hajela, P. 1994: Multidisciplinary structural design optimization. In: Kodiyalam, S.; Saxena, M. (eds.) Geometry and optimization techniques for structural optimization, pp. 363-386. Elsevier Applied Science
120. Hajela, P.; Lee, J. 1995: Genetic algorithms in multidisciplinary rotor blade design. Proc. 36th AIAA/ASME/ASCE/AHS/ASC SDM Conf. (held in New Orleans, LA), AIAA Paper No. 95-1144, pp. 2187-2197
121. Hajela, P.; Lee, J. 1992: Role of emergent computing techniques in multidisciplinary design. NATO ARW on Emergent Computing Methods in Engineering Design. 4th AIAA/USAF/NASA/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Clevel and, OH)
122. Hajela, P.; Bloebaum, C.L.; Sobieszczanski-Sobieski, J. 1990: Application of global sensitivity equations in multidisciplinary aircraft synthesis. J. of Aircraft 27, 1002-1010
123. Hale, M.A.; Craig, J.I. 1995: On the development of a computing infrastructure that facilitates integrated product and process development from a decision-based design perspective. Proc. First AIAA Aircraft Engineering, Technology, and Operations Cong. (held in Anaheim, CA). AIAA Paper No. 95-3880
124. Harn, Y.-W.; Kabuli, G.M.; Kosut, R.L. 1993: Optimal simultaneous control and structure design. Proc. American Control Conf., Vol. 2, IEEE, pp. 1442-1447
125. Harry, D. 1992: Optimization in solid rocket booster application. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH), AIAA Paper No. 92-4688, pp. 33-40
126. He, C.J.; Peters, D.A. 1992: Optimization of rotor blades for combined structural, dynamic, and aerodynamic properties. Struct. Optim. 5, 37-44
127. He, C.J.; Peters, D.A. 1993: Optimum rotor interdisciplinary design with a finite state aeroelastic system. Mathematical & Computer Modelling 18
128. Henderson, J.L.; Gürdal; Z.; Loos, A.C. 1996: Combined structural and manufacturing optimization of stiffened composite panels. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 999-1009. AIAA Paper No. 96-4093
129. Herendeen, D.; Ludwing, M.; Marco, J.S. 1992: The impact of database technology on multidisciplinary design optimization. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4831
130. Hirsch, U.; Kuntze, H.-B.; Brecht, R.; Kilthau, A. 1992: Structure and parameter optimization of an active absorber for decentralized vibration control. Proc. 1992 IEEE Int. Conf. on Robotics and Automation 1, 670-675
131. Hoadley, S.T.; Karpel, M. 1991: Application of aeroservoelastic modeling using minimum-state unsteady aerodynamic approximations. J. Guidance, Control, & Dynamics 14, 1267-1276
132. Huang, X.; Dudley, J.; Haftka, R.T.; Grossman, B.; Mason, W.H. 1996: Structural weight estimation for multidisciplinary optimization of a high-speed civil transport. J. Aircraft 33, 608-616
133. Hulme, K.F.; Bloebaum, C.L.: 1996: Development of Cascade: A multidisciplinary design test simulator. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 438-447. AIAA Paper No. 96-402
134. Hutchison, M.G.; Unger, E.R.; Mason, W.M.; Grossman, B.; Haftka, R.T. 1994: Variable complexity aerodynamic optimization of a high-speed civil transport wing. J. Aircraft 31, 110-120
135. Ide, H.; Abdi, F.F.; Shankar, V.J. 1988: CFD sensitivity study for aerodynamic/control optimization problems. AIAA Paper 88-2336
136. James, B.B. 1993: Multidisciplinary optimization of a controlled space structure using 150 design variables. NASA CR-4502
137. Jayaram, S.; Myklebust, A.; Gelhausen, P. 1992: ACSYNT - A standards-based system for parametric computer aided conceptual design of aircraft. AIAA Paper 92-1268
138. Jin, I.M.; Sepulveda, A.E. 1995: Structural/control system optimization with variable actuator masses. AIAA J. 33, 1709-1714
139. Johnson, E.; Brockman, J. 1996: Reducing overall design time through efficient allocation of individual task times Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4159
140. Johnson, E.W.; Brockman, J.B. 1995: Incorporating design schedule management into a flow management system. Proc. 32nd IEEE/ACM Design Automation Conf. (held in San Francisco, CA)
141. Johnson, W.: 1988: A comprehensive analytical model of rotorcraft aerodynamics and dynamics-Johnson Aeronautics version. Volume II: user's manual: CAMRAD/JA. Palo Alto, CA: Johnson Aeronautics
142. Jones, K. 1992: Information management for large multidisciplinary project. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4720
143. Junkins, J.L.; Rew, D.W. 1988: Unified optimization of structures and controllers. In: Atluri, S.N.; Amos, A.K. (eds.) Large space structures dynamics and control. Berlin, Heidelberg, New York: Springer
144. Kajiwara, I.; Nagamatsu, A.; Seki, K.; Kotani, Y. 1996: Integrated optimum design of structure and servosystem with dynamic compensator. AIAA/ASME/ASCE/AHS/ ASC 37th Structures, Structural Dynamics, and Materials Conf. (held in Salt Lake City, UT). AIAA Paper No. 96-1433
145. Karandikar, H.M.; Mistree, F. 1993: Modeling concurrency in the design of composite structures. In: Kamat, M.P. (ed.) Structural optimization: status and promise, pp. 769-806. Washington, D.C.: AIAA
146. Karpel, M. 1992a: Multidisciplinary optimization of aeroservoelastic systems using reduced-size models. J. of Aircraft 29, 939-946
147. Karpel, M. 1992b: Size reduction techniques for the determination of efficient aeroservoelastic models. In: Leondes, C. (ed.) Control and dynamic systems-advances in theory and applications 54, pp. 263-295. New York: Academic Press
148. Karpel, M. 1996: Modal-based enhancement of integrated structural design optimization schemes. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 1223-1232. AIAA Paper No. 96-4126
149. Kaufman, M.; Balabanov, V.; Burgee, S.L.; Giunta, A.A.; Grossman, B.; Haftka, R.T.; Mason, W.H.; Watson, L.T. 1996: Variable-Complexity Response Surface Approximations for Wing Structural Weight in HSCT Design. Computational Mechanics 18(2), 112-126
150. Khalak, H.; Miller, R.; Weeks, C.; Bloebaum, C. L. 1994: Simulated annealing applied to molecular structure determination. Proc. 5th AIAA Multidisciplinary Analysis and Optimization Symp. (held in Panama City, FL). AIAA Paper No. 94-4352
151. Khot, N.S.; Abhyankar, N.S. 1993: Integrated optimum structural and control design. In: Kamat, M.P. (ed.) Structural optimization: status and promise, p. 743. Washington, D.C.: AIAA
152. Khot, N.S.; Eastep, F.E.; Kolonay, R.M. 1996: Optimization of a composite wing structure for enhancement of the rolling maneuver. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 152-161. AIAA Paper No. 96-3998
153. Kincaid, R.K.; Barger, R.T. 1993: The damper placement problem on space truss structures. Location Science 1, 219-234
154. King, E.G.; Freeman, L.M.; Whitaker, K.W.; Karr, C.L. 1991: Two-dimensional thrust vectoring nozzle optimization techniques. 29th Aerospace Sciences Meeting (held in Reno, Nevada). AIAA Paper No. 91-0473
155. Kirk, J. 1992: The use of multivariate analysis to optimize design parameters for extended- range combat aircraft. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA 92-4707-CP, Part 1, pp. 159-167
156. Kirsch, U. 1981: Optimum structural design. McGraw-Hill
157. Kirsch, U. 1991: Reduced basis approximations of structural displacements for optimal design. AIAA J. 29, 1751-1758
158. Kisielewicz, L.T. 1989: The INGECAD multidisciplinary integrated computer aided engineering system. Nuclear Engineering & Design 111, 233-241
159. Kodiyalam, S., Vanderplaats, G.N. 1989: Shape optimization of 3D continuum structures via force approximation technique. AIAA J. 27, 1256-1263
160. Kolonay, R.; Venkayya, V.; Yang, H. 1994: Sensitivity analysis for transonic unsteady aeroelastic constraints. 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA-94-4263
161. Korivi, V.M.; Newman, P.A.; Taylor, A.C. 1994: Aerodynamic optimization studies using a 3-D supersonic Euler code with efficient calculation of
162. Korngold, J.; Gabriele, G. 1994: Integrating design for manufacturing of electronic packages in a multidisciplinary design analysis and optimization framework. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4254
163. Korngold, J.; Gabriele, G.; Renaud, J.; Kott, G. 1992: Application of multidisciplinary design optimization to electronics package design. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA 92-4704-CP, Part 1
164. Koval, L.R. 1980: Sound transmission into a laminated composite cylindrical shell. J. Sound & Vib. 71
165. Kroo, I. 1995: Decomposition and collaborative optimization for large scale aerospace design. ICASE/LaRC/SIAM Workshop on Multidisciplinary Optimization (held in Hampton, VA). Also to appear in SIAM J., 1996
166. Kroo, I. 1995: Decomposition and collaborative optimization for large scale aerospace design. ICASE/LaRC/SIAM Workshop on Multidisciplinary Optimization (held in Hampton, VA). Also to appear in SIAM J., 1996
167. Kroo, I.; Altus, S.; Braun, R.; Gage, P.; Sobieski, J. 1994: Multidisciplinary optimization methods for aircraft preliminary design. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL), Vol. 1. AIAA Paper No. 94-4325, pp. 697-707
168. Kroo, I.; Takai, M. 1988a: A quasi-procedural knowledge-based system for aircraft synthesis. AIAA Aircraft Design Conf., AIAA Paper No. 88-6502
169. Kroo, I.; Takai, M. 1988b: Quasi-procedural knowledgebased system for aircraft design. AIAA Paper No. 88-4428
170. Kroo, I.; Takai, M. 1990: Aircraft design optimization using a quasi-procedural method and expert system. Proc. 3rd AIAA/NASA/USAF/OAI Symp. Multidisciplinary Analysis and Optimization (held in San Francisco, CA)
171. Ku, C.-S.; Hajela, P. 1995: Dual structural-control design of an adaptive neurocontroller for airfoil vibration reduction. Proc. Int. Federation of Operations Research Societies (IFORS), 4th Specialized Conf. on Operations Research and Engineering Design (held in St.-Louis, MO)
172. Kuo, C.-P.; Bruno, R. 1991: Optimal actuator placement on an active reflector using a modified simulated annealing technique. Proc. First Joint U.S./Japan Conf. on Adaptive Structures (held Maui, Hawaii), pp. 1056-1067. Technomic Publishing Co., Inc.
173. Kusiak, A; Larson, T. Nick; Wang, J. 1994: Reengineering of design and manufacturing processes. Computers Industrial Engineering 26, 521-536
174. Lamancusa, J.S. 1993: Numerical optimization techniques for structural-acoustic design of rectangular panels. Comp. & Struct. 48, 661-675
175. Lamancusa, J.; Eschenauer, H. 1992: Design optimization methods for rectangular panels with minimal sound radiation. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4768
176. Lautenschlager, U.; Erikstad, S.O.; Allen, J.K.; Mistree, F. 1995: Experimental trajectory analysis using decision based robust design. AIAA J. Guidance, Control, & Dynamics 18, 1126-1133
177. Lasdon, L.S. 1970: Optimization theory of large systems. New York: Macmillan
178. Lavelle, T.; Plencner, R. 1992: Concurrent optimization of airframe and engine design. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4713
179. Lee, H.; Goel, S.; Tong, S.S.; Gregory, B.; Hunter, S. 1993: Toward modeling the concurrent design of aircraft engine turbines. Int. Gas Turbine and Aeroengine Cong. and Exposition (held in Cincinnati, OH), Paper ASME 93-GT-193
180. Lee, J.; Hajela, P. 1995: Parallel genetic algorithm implementation in multidisciplinary rotor blade design. Proc. AHS Specialists Meeting (held in Williamsburg, VA). Also to appear in J. of Aircraft
181. Lepsch, R. A.; Stanley, D.O.; Unal, R. 1995: Application of dualfuel propulsion to a single stage AMLS vehicle. J. Spacecraft & Rockets 32, 417-425. Also AIAA Paper No. 93-2275, 1993
182. Lewis, K.; Mistree, F. 1995: Designing top-level aircraft specifications: A decision-based approach to a multiobjective, highly constrained problem. 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf. (held in New Orleans, LA). AIAA-95-1431-CP, pp. 2393-2405
183. Lewis, M.L. 1996: A trust region framework for managing approximation models in structural optimization. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 1053-1055. AIAA Paper No. 96-4101
184. Li, W-L.; Livne, E. 1995: Supersonic/subsonic lifting surface unsteady aerodynamic sensitivities and approximations for aeroservoelastic shape optimization. To appear in J. of Aircraft
185. Librescu, L.; Meirrovitch, L.; Song, O. 1996: Integrated structural tailoring and control using adaptive materials for advanced aircraft wings. J. of Aircraft 33, 203-213
186. Lim, J.W.; Chopra, I. 1991: Aeroelastic optimization of a helicopter rotor using an efficient sensitivity analysis. J. of Aircraft 28, pp. 29-37
187. Livne, E. 1989: Accurate calculation of control augmented structural eigenvalue sensitivities using reduced order models. AIAA J. 27, 947-954
188. Livne, E. 1993: Alternative approximations for integrated control/structure aeroservoelastic synthesis. AIAA J. 31, 1100-1112
189. Livne, E.; Li, W.-L. 1995: Aeroservoelastic aspects of wing/control surface planform shape optimization. AIAA J. 33, 302-311
190. Livne, E.; Friedmann, P.P.; Schmit, L.A. 1992: Integrated aeroservoelastic wing synthesis by nonlinear programming/approximation concepts. J. Guidance, Control, & Dynamics 15, 985-997
191. Livne, E.; Schmit, L.A.; Friedmann, P.P. 1990: Towards integrated multidisciplinaiy synthesis of actively controlled fiber composite wings. AIAA J. of Aircraft 27, 979-992
192. Livne, E.; Schmit, L.A.; Friedmann, P.P. 1992: Exploratory design studies of actively controlled wings using integrated multidisciplinary synthesis. AIAA J. 30, 1171-1183
193. Livne, E.; Schmit, L.A.; Friedmann, P.P. 1993: Integrated structure/control/aerodynamic synthesis of actively controlled composite wings. J. of Aircraft 30, 387-394
194. Logan, T.R. 1990: Strategy for multilevel optimization of aircraft. J. of Aircraft 27, 1068-1072
195. Lokanathan, A.; Brockman, J.B.; Renaud, J.E. 1995: A multidisciplinary optimization approach to integrated circuit design. Proc. Concurrent Engineering: A Global Perspective, CE95 Conf. (held in McLean, VA), pp. 121-129
196. Lokanathan, A.N.; Brockman, J.B.; Renaud, J.E. 1996: Concurrent design of manufacturable intgegrated circuits. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 1010-1018. AIAA Paper No. 96-4094
197. Longacre, K., Vance, J., Devries, R.1996: A computer tool to facilitate cross-attribute optimization. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4132
198. Longo, A.; No, M.; Aizpitarte, M.; Unzueta, J. 1991: Conservative approximations in nonlinear optimization: theory and examples. Comp. & Struct. 30, 441-449
199. Luo, X.; Rajagopalan, H.S.; Grandhi, R.V. 1996: MIDAS: Multidisciplinary interactive design and analysis system-integration of ASTROS and I-DEAS. Proc. 37th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conf., Part 3 (held in Salt Lake City, UT). AIAA Paper 96-1504, pp. 1665-1679
200. Malone, B.; Mason, W.H. 1992: Aircraft concept optimization using the global sensitivity approach and parametric multiobjective figures of merit. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleve land, OH). AIAA Paper No. 92-4221
201. Malone, B.; Mason, W.H. 1991: Multidisciplinary optimization in aircraft design using analytic technology models. AIAA Paper No. 91-3187
202. Mars, W.J.; Mavris, D.N.; Schrage, D.P. 1996: Effects of alternative wing structural concepts on high speed civil transport life cycle cost. Proc. 37th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics and Materials Conf., Part 1 (held in Salt Lake City, UT). AIAA Paper 96-1381, pp. 562-582
203. Marx, W.; Mavris, D.; Schrage, D. 1994: Integrated product development for the wing structural design of the high-speed civil transport. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA-94-4253
204. Mason, B.H.; Haftka, R.T.; Johnson, E.R. 1994: Analysis and design of composite channel frames. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper 94-4364-CP, Vol. 2, pp. 1023-1040
205. Mason, W.H.; Arledge, T.K. 1993: ACSYNT aerodynamic estimation, examination and validation for use in conceptual design. AIAA Paper 93-0973
206. Mavris, D.N.; Bandte, M.; Schrage, D.P. 1996: Application of probabilistic methods for the determination of an economically robust HSCT configuration. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 968-978. AIAA Paper No. 96-4090
207. McCarthy, T.R.; Chattopadhyay, A. 1993: Design of high speed proprotors using multiobjective optimization techniques. Proc. AIAA/AHS/ASEE Aerospace Design Conf. (held in Irvine, CA). AIAA Paper No. 93-1032
208. McCarthy, T.R.; Chattopadhyay, A.; Zhang, S. 1995: A coupled rotor/wing optimization procedure for high speed tilt-rotor aircraft. Presented at 51st AHS Annual Forum (held in Fort Worth, TX)
209. McCullers, L.A. 1984: Aircraft configuration optimization including optimized flight profiles. Proc. Symp. on Recent Experiences in Multidisciplinary Analysis and Optimization, NASA CP-2327, pp. 395-412
210. McCulley, C., Bloebaum, C.L. 1996: Complex system design task sequencing for cost and time considerations. 6th AIAA/USAF/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA)
211. McCulley, C.; Bloebaum, C.L. 1994: Optimal scheduling for complex engineering systems using genetic algorithms. Proc. 5th AIAA Multidisciplinary Analysis and Optimization Symp. (held in Panama City, FL). AIAA Paper No. 94-4327
212. McGeer, T. 1984: Wing design for minimum drag and practical constraints. J. of Aircraft 21, 879-886
213. McQuade, P.D.; Eberhardt, S.; Livne, E. 1995: CFD-based aerodynamic approximation concepts optimization of a two-dimensional scramjet vehicle. J. of Aircraft 32, 262-269
214. Messac, A. 1996: Physical programming: effective optimization for computational design. AIAA J. 34, 149-158
215. Michelena, N.; Papalambros, P. 1995: Optimal model-based decomposition of powertrain system design. Trans. ASME J. Mech. Des. 117, 499-505
216. Miller, G. 1994: An active flexible wing multidisciplinary design optimization method. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4412
217. Millman, M.; Salama, M.; Wette, M. 1991: Integrated controls structure and optical design. Proc. IEEE American Control Conf., Vol. 2, pp. 1448-1452
218. Millman, M.; Salama, M.; Chu, C.C.; Wette, M. 1992: Integrated control-structure design of the JPL phase B testbed. AIAA Aerospace Design Conf. and Exhibit (held in Irvine, CA). AIAA Paper 92-1151
219. Millman, M.; Salama, M.; Scheid, R. 1990: A homotopy approach for combined control- structure optimization: Constructive analysis and numerical examples. AIAA 28th Aerospace Science Meeting (held in Reno, Nevada)
220. Millman, M.; Salama, M.; Scheid, R. E.; Bruno, R.; Gibson, J.S. 1991: Combined control-structural optimization. Comp. Mech. 8, 1-18
221. Mistree, F.; Hughes, O.F.; Bras, B.A. 1993: The compromise decision support problem and the adaptive linear programming algorithm. In: Kamat, M.P. (ed.) Structural optimization: status and promise, pp. 247-286. Washington, D.C.: AIAA
222. Mistree, F.; Smith, W.F.; Bras, B.A. 1993: A decision-based approach to concurrent engineering. In: Paresai, H.R.; Sullivan, W. (eds.) Handbook of concurrent engineering, pp. 127-158. New York: Chapman & Hall
223. Mistree, F.; Smith, W.F.; Bras, B.; Allen, J.K.; Muster, D. 1990: Decision-based design: A contemporary paradigm for ship design. Trans. Soc. Naval Architects & Marine Engineers 98, 565-597
224. Moore, A.A.; Braun, R.D.; Powell, R.W. 1995: The infusion of cost into the multidisciplinary design of space transportation systems. Proc. 17th Annual Conf. Int. Soc. of Parametric Analysts
225. Morris, S.J.; Kroo, I. 1990: Aircraft design optimization with dynamic performance constraints. J. of Aircraft 27, 1060-1067
226. Murthy, D.V.; Haftka, R.T. 1988: Approximations to eigenvalues of modified general matrices. Comp. & Struct. 29, 903-917
227. Nash, S.; Polyak, R.; Sofer, A. 1994: A numerical comparison of barrier and modified barrier methods for large-scale bound-constrained optimization. In: Hager, W.; Hearn, D.; Pardalos, P. (eds.) Large scale optimization: state of the art. Dordrecht: Kluwer
228. Neill, D.J.; Johnson, E.H.; Canfield, R. 1990: ASTROS - A multidisciplinary automated structural design tool. J. of Aircraft 27, 1021-1027
229. Nelson, S.; Papalambros, P. 1996: Sequentially decomposed programming. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4008
230. Nesterov, Y.E.; Nemirovsky, A.S. 1994: Interior point polynomial methods in convex programming: theory and algorithms. SIAM J. Optimiz.
231. Nguyen, V.H.; Fleury, C.; Strodiot, J.J. 1987: A mathematical convergence analysis of the convex linearization method for engineering design optimization. Eng. Opt. 11, 195-216
232. Niu, X.; Brockman, J.B. 1995: A Bayesian approach to variable screening for modeling the IC fabrication process. Proc. IEEE Int. Symp. on Circuits and Systems (held in Seattle, WA)
233. Nowaczyk, R.H.; Levi, D.J 1996: Two approaches to teaching team skills to engineering and science students. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 826-832. AIAA Paper No. 96-4068
234. Nowaczyk, R.H.; Perlow, R.; Palazzo, M.A. 1996: An examination of personality traits and engineering/science student team performance. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 833-837. AIAA Paper No. 96-4069
235. Nystrom, G.; Eason, E.; Wright, J.; Burlingham, A. 1994: A new three-step move limit strategy for non-hierarchic multidisciplinary system optimization. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4331
236. Ohsaki, M.; Arora, J. 1993: A direct application of parametric programming techniques to structural optimization problems. Int. J. Numer. Meth. Engng. 36, 2683-2702
237. Olds, J. 1992: The suitability of selected multidisciplinary design and optimization techniques to conceptual aerospace vehicle design. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4791
238. Olds, J. 1994: System sensitivity analysis applied to the conceptual design of a dual-fuel rocket SSTO. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4339
239. Olds, J.R.; Lee, H. 1996: Application of a new economic analysis tool to a two- stage-to-orbit RBCC launch vehicle design. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 88-998. AIAA Paper No. 96-4092
240. Otto, J.C.; Landman, D.; Patera, A.T. 1996: A surrogate approach to the experimental optimization of multielement airfoils. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 1323-1333. AIAA Paper No. 96-4138
241. Padula, S.L.; Adelman, H.M.; Bailey, M.C.; Haftka, R.T. 1989: Integrated structural electromagnetic shape control of large space antenna reflectors. AIAA J. 27, 814-819
242. Padula, S.L.; Alexandrov, N.; Green, L.L. 1996: MDO test suite at NASA Langley Research Center. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA),pp. 410-420. AIAA Paper No. 96-4028
243. Padula, S.L.; Kincaid, R.K. 1995: Aerospace applications of integer and combinatorial optimization. NASA TM-110210. Also presented at 1995 SIAM Annual Meeting (held in Charlotte, NC) (339 KB)
244. Padula, S.L.; Sandridge, C.A. 1993: Passive/active strut placement by integer programming. In: Topology design of structures, pp. 145-156. Dordrecht: Kluwer
245. Padula, S.L.; James, B.B.; Graves, C.P.; Woodard, S.E. 1991: Multidisciplinary optimization of controlled space structures using global sensitivity equations. NASA TP-3130
246. Padula, S.; Sandridge, C. 1992: Active strut placement using integer programming for the CSI evolutionary model. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4787
247. Papalambros, P.; Michelena, N. 1996: Model-based partitioning in optimal design of large engineering systems. In: Alexandrov, N.; Hussaini, M. (eds.) Multidisciplinary design optimization: state-of-the-art. SIAM
248. Park, J.-H.; Asada, H. 1992: Integrated structure/control design of a two-link nonrigid robot arm for high speed positioning. Proc. IEEE Int. Conf. on Robotics and Automation, Vol. 1, pp. 735-741
249. Parkinson, A.R.; Balling, R.J.; Free, J.C. 1992: OPTDESX: An X window-based optimal design software system. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4759
250. Pates, C.; Anatrol, R.; Shirahatti, U.; Mei, C. 1995: Coupled boundary/finite element methods for random structuralacoustic interaction problems. AIAA/ASME/ASCE/ AHS/ASC 36th Structures, Structural Dynamics, and Materials Conf. (held in New Orleans, LA). AIAA Paper No. 95-1346
251. Pimmler, T.U.; Eppinger, S.D. 1994: Integration analysis of product decompositions. ASME Design Theory and Methodology Conf. (held in Minneapolis, Minnesota)
252. Polyak, R. 1992: Modified barrier functions in LP. IBM Research Report RC 17790 (No. 78331). Yorktown Heights, New York, p. 56
253. Rais-Rohani, M.; Haftka, R.; Grossman, B.; Unger, E. 1992: Integrated aerodynamic- structural-control wing design. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH), Part 1, AIAA 92-469 4-CP, pp. 53-62
254. Rakowska, J.; Haftka, R.T.; Watson, L.T. 1991: Tracing the efficient curve for multi-objective control-structure optimization. Computing Systems in Engng. 2, 461-471
255. Rakowska, J.; Haftka, R.T.; Watson, L.T. 1993: Multi-objective control-structure optimization via homotopy methods. SIAM J. Optimiz. 3, 654-667
256. Rao, S.; Venkayya, V. 1992: Mixed-integer programming and multiobjective optimization techniques for the design of control augmented structures. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4739
257. Reddy, E.; Abumeri, G.; Murthy, P.; Chamis, C. 1992: Structural tailoring of aircraft engine blade subject to ice impact constraints. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4710
258. Renaud, J.E.; Gabriele, G.A. 1993: Improved coordination in nonhierarchic system optimization. AIAA J. 31, 2367-2373
259. Renaud, J.E.; Gabriele, G.A. 1994: Approximation in nonhierarchic system optimization. AIAA J. 32, 198-205,
260. Renaud, J.E.; Gabriele, G.A. 1991: Sequential global approximation in non-hierarchic system decomposition and optimization. In: Gabriele, G. (ed.) Advances in Design Automation and Design Optimization, 19th Design Automation Conf. (held in Miami, FL), ASME Publication DE-Vol. 32-1, pp. 191-200
261. Rogers, J.L.; McCulley, C.M.; Bloebaum, C.L. 1996: Integrating a genetic algorithm into a knowledge-based system for ordering complex design processes. 4th Int. Conf. on Artificial Intelligence in Design 96 (held at Stanford University, Palo Alto, CA)
262. Rogers, J., McCulley, C., Bloebaum, C.L. 1996: Integrating a genetic algorithm into a knowledge-based system for ordering complex design processes. Accepted for 4th Int. Conf. on AI in Design (held in Stanford, CA)
263. Rogers, J.L. 1989: A knowledge-based tool for multilevel decomposition of a complex design problem. NASA TP-2903
264. Rohl, P.; Mavris, D.; Schrage, D. 1995: Combined aerodynamic and structural optimization of a high-speed civil transport wing. AIAA/ASME/ASCE/ AHS/ASC 36th Structures, Structural Dynamics, and Materials Conf. (held in New Orleans, LA). AIAA Paper No. 95-1222
265. Rowan, T.H. 1990: Functional stability analysis of numerical algorithms. Ph.D. Dissertation, Department of Applied Mathematics, The University of Texas at Austin
266. Sacks, J.; Welch, W.J.; Mitchell, T.J.; Wynn, H.P. 1989: Design and analysis of computer experiments. Statistical Science 4 , 409-435
267. Sandridge, C.A.; Haftka, R.T. 1991: Modal truncation, Ritz vectors and damping-ratio derivatives in structural control. J. Guidance, Control, & Dynamics 14, 785-790
268. Schmit, L.A. 1984: Structural synthesis-precursor and catalyst. Recent experiences in multidisciplinary analysis and optimization. NASA CP-2337, Part 1, pp. 1-17
269. Schmit, L.A., Jr.; Farshi, B. 1974: Some approximation concepts for structural synthesis. AIAA J. 12, 692-699
270. Schmit, L.A.; Ramanathan, R.K. 1978: Multilevel approach to minimum weight design including buckling constraints. AIAA J. 16, 97-104
271. Schneider, G.; Krammer, J.; Hoernlein, H.R. 1991: First approach to an integrated fin design. Proc. 72nd Meeting of the Structures and Materials Panel (held in Bath, UK). Also in Integrated design analysis and optimization of aircraft structures, AGARD Report 784, 1992
272. Schneider, G.; Krammer, J.; Hoernlein, H.R. 1991: First approach to an integrated fin design. Proc. 72nd Meeting of the Structures and Materials Panel (held in Bath, UK). Also in Integrated design analysis and optimization of aircraft structures, AGARD Report 784, 1992
273. Schrage, D. 1993: Concurrent design: a case study. In: Kusiak, A. (ed.) Concurrent engineering, automation, tools, techniques, pp. 535-581. J. Wiley & Sons
274. Schweiger, J., Krammer, J., Hornlein, H. 1996 Development and application of the integrated structural design tool LAGRANGE. Proc. 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4169
275. Scotti, S. J. 1993: Structural design utilizing updated approximate sensitivity derivatives. AIAA Paper No. 93-1531
276. Scotti, S.J. 1995: Structural design using equilibrium programming. Ph.D. Dissertation, Extension at NASA LaRC, George Washington University
277. Seller, R.; Batill, S. 1996: Concurrent subspace optimization using gradient-based neural network approximations. Proc. 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4019
278. Sellar, R.S.; Batill, S.M.; Renaud, J.E. 1996: Response surface based, concurrent subspace optimization for multidisciplinary system design. 34th AIAA Aerospace Sciences Meeting (held in Reno, Nevada). AIAA 96-0714
279. Sepulveda, A.; Jin, I. 1995: Design of structure/control systems with transient response constraints exhibiting relative minima. Struct. Optim. 10, 167-172
280. Seus, R.H.; Oakley, D.R.; Rhodes, G.S.; Hopkins, D.S. 1996: MDO of Aeropropulsion Components Considering Uncertainty. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 776-784. AIAA Paper No. 96-4062
281. Shankar, J.; Ribbens, C.J.; Haftka, R.T.; Watson, L.T. 1993: Computational study of a nonhierarchical decomposition algorithm. Comput. Optim. Appl. 2, 273-293
282. Shirk, H.M.; Hertz, T.Z.; Weisshaar, T.A. 1986: A survey of aeroelastic tailoring - Theory, practice, and promise. J. of Aircraft 23, 6-8
283. Shupe, J.; Srinivasan, R. 1992: Decision based product improvement: the importance of multidisciplinary decision making to product development. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH), Part 1. AIAA Paper No. 92-4706, pp. 148-58
284. Smith, R.; Kerr, P. 1992: Geometric requirements for multidisciplinary analysis of aerospace-vehicle design. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4773
285. Snyman, J.A.; Fatti, L.P. 1987: A multi-start global minimization algorithm with dynamic search trajectories. J. Optim. Theory Appl. 54, 121-141
286. Sobieski, I.P.; Kroo, I. 1996: Collaborative optimization applied to an aircraft design problem. AIAA Aerospace Sciences Meeting (held in Reno, Nevada). AIAA Paper No. 96-0715
287. Sobieski, J.; Gross, D.W.; Kurtze, W.L.; Newsom, J.R.; Wrenn, G.A.; Greene, W.H. 1979: Supersonic cruise research aircraft structural studies, methods, and results. Proc. Supersonic Cruise Aircraft Research Conf. (held in Hampton, VA)
288. Sobieszczanski-Sobieski, J. 1982a: From a black box to a programming system. In: Morris, A.J. (ed.) Foundations of structural optimization: a unified approach. J. Wiley & Sons
289. Sobieszczanski-Sobieski, J. 1982b: A linear decomposition method for large optimization problems - Blueprint for development. NASA TM-83248
290. Sobieszczanski-Sobieski, J. 1986: The case for aerodynamic sensitivity analysis. Sensitivity analysis in engineering. NASA CP-2457, pp. 77-96
291. Sobieszczanski-Sobieski, J. 1988: Optimization by decomposition: a step from hierarchic to non-hierarchic systems. Presented at the Second NASA/Air Force Symp. on Recent Advances in Multidisciplinary Analysis and Optimization (held in Hampton, VA), N ASA CP-3031, Part 1. Also NASA TM-101494
292. Sobieszczanski-Sobieski, J. 1990a: Sensitivity of complex, internally coupled systems. AIAA J. 28, 153-160
293. Sobieszczanski-Sobieski, J. 1990b: Higher order sensitivity analysis of complex, coupled systems. AIAA J. 28, 736
294. Sobieszczanski-Sobieski, J. 1993: Optimization by decomposition in structural and multidisciplinary optimization. In: Rozvany, G.I.N. (ed.) Optimization of large structural systems, Vol. 1, pp. 193-234. Dordrecht: Kluwer
295. Sobieszczanski-Sobieski, J. 1995: Multidisciplinary design optimization: an emerging, new engineering discipline. In: Herskovits, J. (ed.) Advances in structural optimization, pp. 483-496. Dordrecht: Kluwer
296. Sobieszczanski-Sobieski, J.; Barthelemy, J.-F.M.; Riley, K.M. 1992: Sensitivity of optimum solutions to problems parameters. AIAA J. 20, 1291-1299
297. Sobieszczanski, J.; Loendorf, D. 1972: A mixed optimization method for automated design of fuselage structures. J. Aircraft
298. Sobieszczanski, J.; McCullers, L.A.; Ricketts, R.H.; Santoro, N.J.; Beskenis, S.D.; Kurtze, W.L. 1976: Structural design studies of a supersonic cruise arrow wing configuration. Proc. Supersonic Cruise Aircraft Research Conf. (held in Hampton, VA), NASA CP-001, p. 45
299. Sobieszczanski-Sobieski, J.; Bloebaum, C.L.; Hajela, P. 1988: Sensitivity of control augmented structure obtained by a system decomposition method. AIAA Paper 88-2205
300. Sobieski, I.; Kroo, I.; Braun, R.; Gage, P. 1996: Implementation and performance issues in collaborative optimization. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4017
301. Stanley, D.; Unal, R.; Joyner. R. 1992: Applicaton of Taguchi methods to dual mixture ratio propusion system optimization for SSTO vehicles. AIAA 30th Aerospace Sciences Meeting and Exhibit (held in Reno, Nevada). AIAA Paper 92-0213
302. Stanley, D.O.; Engelund, W.C.; Lepsch, R.A.; McMillin, M.; Wurster, K.E.; Powell, R.W.; Guinta, A.A.; Unal, R. 1994: Rocket-powered single-stage vehicle configuration selection and design. J. of Spacecraft & Rockets 31. Also AIAA Paper No. 93-1053, 1993
303. Stanley, D.O.; Engelund, W.C.; Lepsch, R.A.; McMillin, M.; Wurster, K.E.; Powell, R.W.; Guinta, A.A.; Unal, R. 1994: Rocket-powered single-stage vehicle configuration selection and design. J. of Spacecraft & Rockets 31. Also AIAA Paper No. 93-1053, 1993
304. Starnes, J.H., Jr.; Haftka, R.T. 1979: Preliminary design of composite wings for buckling, stress and displacement constraints. J. of Aircraft 16, 564-570
305. Stettner, M.; Mavris, D.N.; Schrage, D.P. 1996: A method for flexible design integration. Proc. 37th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conf. (held in Salt Lake City, UT). AIAA 96-1540
306. Steward, D.V. 1991: Systems analysis and management: structure, strategy, and design. Petrocelli Books, Inc.
307. Storaasli, O.O.; Sobieszczanski, J. 1973: Design oiented structural analysis. AIAA/ASME/SAE 14th Structures, Structural Dynamics, and Materials Conf. (held in Williamsburg, VA). AIAA Paper No. 73-338
308. Sutjahjo, E.; Chamis, C. 194: Multidisciplinary coupled finite element procedures for fluid mechanics, heat transfer, and solid mechanics. AIAA/NASA/USAF/ISSMO 5th Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4256
309. Suzuki, S. 1993: Simultaneous structure/control design optimization of a wing structure with a gust load alleviation system. J. of Aircraft 30, 268-274
310. Suzuki, S.; Matsuda, S. 1991: Structure/control design synthesis of active flutter suppression system by goal programming. AIAA J. Guidance, Control, & Dynamics 14, 1260-1266
311. Suzuki, S. 1995: Multigoal programming for structure/control design synthesis with fuzzy goals. JSME Int. J. 38, 450-456
312. Suzuki, S.; Kawamura, N. 1996: Simultaneous optimization of sailplane design and its flight trajectory. J. Aircraft 33, 567-571
313. Szewczyk, Z.P.; Hajela, P. 1994: Neurocomputing strategies in structural design - Decomposition based optimization. Struct. Optim. 8, 242-250
314. Tai, J.C.; Mavris, D.N.; Schrage, D.P. 1995: Application of a response surface method to the design of tipjet driven stopped rotor/wing concepts. 1st AIAA Aircraft Engineering, Technology, and Operations Cong. (held in Los Angeles, CA). AIAA Paper 95-39 65
315. Thareja, R.; Haftka, R.T. 1990: Efficient single-level solution of hierarchical problems in structural optimization. AIAA J. 28, 506-514
316. Thornton, E.A. 1992: Thermal structures: four decades of progress. J. of Aircraft 20, 485-498
317. Torczon, V. 1993: On the convergence of pattern search methods. Rice University Technical Report TR93-10
318. Torenbeek, E. 1992: Development and application of a comprehensive, design-sensitive weighty prediction method for wing structures of transport category aircraft. Report LR-693, Delft University of Technology, The Netherlands
319. Toropov, V.; Markine, V.L. 1996: The Use of simplified numerical models as mid-range approximations. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 952-958. AIAA Paper No. 96-4088
320. Toropov, V.V.; van Keulen, F.; Markine, V. L.; de Boer, H.: Refinements in the Multi-point approximation method to reduce the effects of noisy structural response. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 941-951. AIAA Paper No. 96-4087
321. Trebilcock, R.; Morris, A. 1996: Methodology for optimum design for military airframes. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4128
322. Tulinius, J. 1992: Multidisciplinary optimization is key to integrated product development process. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH)
323. Tyll, J.S.; Eaglesham, M.A.; Schetz, J.A.; Deisenroth, M.; Mook, D.T. 1996: An MDO design methodology for the concurrent aerodynamic/cost design of Maglev vehicles. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 501-513. AIAA Paper No. 96-4036
324. Tzong, G.; Baker, M.; D-Vari, R.; Giesing, J. 1994: Aeroelastic loads and structural optimization of a high speed civil transport model. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4378
325. Unal, R.; Lepsch, R.; Engelund, W.; Stanley, D. 1996: Approximation model building and multidisciplinary design optimization using response surface methods. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4044
326. Unal, R.; Stanley, D.O.; Engelund, W.C.; Lepsch, R.A.; McMillin, M.M. 1993: Design for quality using response surface methods. Proc. 14th Annual Conf. of the American Society for Engineering Management, pp. 7-11
327. Unal, R.; Stanley, D.O. 1993: Parametric design optimization using response surface methods. Proc. 15th Annual Conf. Int. Soc. of Parametric Analysts, Vol. XII, pp. 87-96
328. Unger, E.R.; Hall, L.E. 1994: The use of automatic differentiation in an aircraft design problem. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA 94-4260-CP, Vol. 1, pp. 64-72
329. Unger, E.R.; Hutchison, M.G.; Rais-Rohani, M.; Haftka, R.T.; Grossman, B. 1992a: Variable-complexity multidisciplinary design of a transport wing. Int. J. System Automation: Research and Applications (SARA) 2, 87-113
330. Unger, E. 1994: The use of automatic differentiation in an aircraft design problem. 5th AIAA/ USAF/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Paper No. 94-4260
331. Unger, E.; Hutchison, M.; Huang, X.; Mason, W.; Haftka, R.; Grossman, B. 1992b: Variable-complexity aerodynamic-structural design of a high-speed civil transport. Proc. 4th AIAA/NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4695
332. Vadde, S.; Allen, J.K.; Mistree, F. 1994: Modeling uncertainty in the combined kinematic and dynamic synthesis of a four-bar linkage. Eng. Opt. 23, 1-15
333. Vanderplaats, G. 1976: Automated optimization techniques for aircraft synthesis. Paper 76-909
334. Vanderplaats, G.N. 1985: ADS: A FORTRAN program for automated design synthesis. Goleta, CA: VMA Engineering, Inc.
335. Veley, D.E.; Rao, S.S. 1996: Multiobjective piezoelectrically damped structures. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Bellevue, WA), pp. 857-865. AIAA Paper No. 96-4074
336. Venkayya, V.B. 1989: Optimality criteria: a basis for multidisciplinary optimization. Comp. Mech. 5, 1-21
337. Volk, J.A. 1992: Multidisciplinary design environment development for air vehicle engineering. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA 92-1113-CP, Part 1, pp. 141-147
338. Wakayama, S.; Page, M.; Liebeck, R. 1996: Mulidisciplinary optimization on an advanced composite wing. Proc. 6th AIAA/NASA/ISSMO Symp. on Multidisciplinary Analysis and Optimization, Part I (held in Bellevue, WA). Also available as AIAA Paper 96-4003
339. Wakayma, S.; Kroo, I. 1992: A method for lifting surface design using nonlinear optimization. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-3292
340. Wakayma, S.; Kroo, I. 1994: Subsonic wing design using multidisciplinary optimization. Proc. 5th AIAA/NASA/USAF/ISSMO Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA 94-4409-CP, Vol. 2, pp. 1358-1368
341. Wagner, T.; Papalambros, P. 1993: A general framework for decomposition analysis in optimal design. In: Gilmore, B.J. (ed.) Advances in design automation, Vol. 2, pp. 315-325. New York: ASME
342. Walsh, J.L. 1987: Optimization procedure to control the coupling of vibration modes in flexible space structures. NASA TM-89115
343. Walsh, J.L. 1988: Experiences in applying optimization techniques to configurations for the control of flexible structures (COFS) program. NASA TM-101511
344. Walsh, J.L.; LaMarsh, W.J.; Adelman, H.M. 1993: Fully integrated aerodynamic/dynamic optimization of helicopter blades. Mathematical and Computer Modelling 18, 53-72
345. Walsh, J.L.; Young, K.C.; Pritchard, J.I.; Adelman, H.M.; Mantay, W.R. 1995: Integrated aerodynamic/dynamic/structural optimization of helicopter rotor blades using multilevel decomposition. NASA TP-3465; ARL Technical Report 518
346. Weisshaar, T.A.; Newsom, J.R.; Gilbert, M.G.; Zeiler, T.A. 1986: Integrated structure/control design - present methodology and future opportunities. ICAS-86-4.8.1
347. Weston, R.P.; Eidson, T.M.; Townsend, J.C.; Coates, R.L. 1994: Distributed computing environment for multidisciplinary optimal design. AIAA/NASA/USAF/ISSMO 5th Symp. on Multidisciplinary Analysis and Optimization (held in Panama City Beach, FL). AIAA Pa per No. 91-4372
348. Woyak, S.A.; Malone, B.; Myklebust, A. 1995: An architecture for creating engineering applications: the dynamic integration system. ASME Computers in Engineering
349. Wrenn, G.A.; Dovi, A.R. 1987: Multilevel decomposition approach to the preliminary sizing of a transport aircraft wing. AIAA 87-0714-CP
350. Wrenn, G.A.; Dovi, A.R. 1988: Multilevel decomposition approach to the preliminary sizing of a transport aircraft wing. AIAA J. of Aircraft 25, 632-638
351. Wujek, B.A.; Renaud J.E.; Johnson E.W.; Brockman, J.B.; Batill, S.M. 1996: Design flow management and multidisciplinary design optimization in application to aircraft concept sizing. 34th AIAA Aerospace Sciences Meeting and Exhibit (held in Reno, Nevada). AIAA 96-0713
352. Wujek, B.A.; Renaud, J.E.; Batill. S.M.; Brockman, J.B. 1995: Concurrent subspace optimization using design variable sharing in a distributed computing environment. In: Azarm, S. (ed) Proc. Design Engineering Technical Conf., Advances in Design Auto motion, ASME DE-Vol. 82, pp. 181-188
353. Yamakawa, H. 1992: Simultaneous optimization of nonlinear structural and control systems. Proc. 4th AIAA/NASA/USAF/OAI Symposium on Multidisciplinary Analysis and Optimization (held in Cleveland, OH). AIAA Paper No. 92-4742
354. Yeh, C.-P.; Fulton, R. 1992: A multidisciplinary approach for PWB design process optimization. Proc. 4th AIAA/ NASA/USAF/OAI Symp. on Multidisciplinary Analysis and Optimization (held in Cleveland, OH), Part 1. AIAA Paper No. 92-4702, pp. 110-118
355. Yuan, K.-A.; Friedmann, P.P. 1995: Structural optimization for vibration reduction of composite helicopter rotor blades with advances geometry tips subject to multidisciplinary constraints. Proc. American Helicopter Soc. 51st Annual Forum (held in Fort Worth, TX), pp. 937-956
356. Yurkovich, R. 1995: Optimum wing shape for an active flexible wing. AIAA/ASME/ ASCE/AHS/ASC 36th Structures, Structural Dynamics, and Materials Conf. (held in New Orleans, LA). AIAA Paper No. 95-1200