-
1
-
-
0019926834
-
-
Ashley, H. (1982), "On making things the best-aeronautical uses of optimization", Journal of Aircraft, Vol. 19 No. 1, pp. 5-28.
-
(1982)
On Making Things the Best-aeronautical Uses of Optimization", Journal of Aircraft
, vol.19
, Issue.1
, pp. 5-28
-
-
Ashley, H.1
-
2
-
-
0001224924
-
Free vibration of composite beams - An exact method using symbolic computation"
-
Banerjee, J.R. and Williams, F.W. (1995), "Free vibration of composite beams - an exact method using symbolic computation". Journal of Aircraft, Vol. 32 No. 3, pp. 636-42.
-
(1995)
Journal of Aircraft
, vol.32
, Issue.3
, pp. 636-642
-
-
Banerjee, J.R.1
Williams, F.W.2
-
3
-
-
85002791931
-
-
Bartholomew, P. and Wellen, H.K. (1990), "Computer-aided optimization of aircraft structures", Journal of Aircraft, Vol. 27 No. 12, pp. 1079-86.
-
(1990)
Computer-aided Optimization of Aircraft Structures", Journal of Aircraft
, vol.27
, Issue.1
, pp. 1079-1086
-
-
Bartholomew, P.1
Wellen, H.K.2
-
4
-
-
8644234033
-
-
5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL
-
Bartholomew, P., Harris, J. and Wellen, H.K. (1994), "The integration of local design of composite panels into overall structural design", 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, pp. 957-65.
-
(1994)
The Integration of Local Design of Composite Panels into Overall Structural Design"
, pp. 957-965
-
-
Bartholomew, P.1
Harris, J.2
Wellen, H.K.3
-
5
-
-
85002924238
-
-
Berkes, U.L (1990), "Efficient optimization of aircraft structures with a large number of design variables", Journal of Aircraft, Vol. 7 No. 12, pp. 1073-8.
-
(1990)
Efficient Optimization of Aircraft Structures with A Large Number of Design Variables", Journal of Aircraft
, vol.7
, Issue.12
, pp. 1073-1078
-
-
Berkes, U.L.1
-
6
-
-
0023167129
-
PANDA2 -program for minimum weight design of stiffened, composite, locally buckled panels"
-
Bushnell, D. (1986), "PANDA2 -program for minimum weight design of stiffened, composite, locally buckled panels". Computers & Structures, Vol. 25 No. 4, pp. 469-605.
-
(1986)
Computers & Structures
, vol.25
, Issue.4
, pp. 469-605
-
-
Bushnell, D.1
-
7
-
-
0029305851
-
Optimum design of composite stiffened wing panels - A parametric study"
-
Butler, R. (1995), "Optimum design of composite stiffened wing panels - a parametric study". The Aeronautical Journal, Vol. 99 No. 985, pp. 169-77.
-
(1995)
The Aeronautical Journal
, vol.99
, Issue.985
, pp. 169-177
-
-
Butler, R.1
-
8
-
-
0030196564
-
-
Butler, R. and Banerjee, J.R. (1996), "Optimum design of bending-torsion coupled beams with frequency or aeroelastic constraints", Computers & Structures, Vol. 60 No. 5, pp. 715-24.
-
(1996)
Optimum Design of Bending-torsion Coupled Beams with Frequency or Aeroelastic Constraints", Computers & Structures
, vol.60
, Issue.5
, pp. 715-724
-
-
Butler, R.1
Banerjee, J.R.2
-
9
-
-
0026861361
-
Optimum design using VICONOPT, a buckling and strength constraint program for prismatic assemblies of anisotropic plates"
-
Butler, R. and Williams, F.W. (1992), "Optimum design using VICONOPT, a buckling and strength constraint program for prismatic assemblies of anisotropic plates". Computers & Structures, Vol. 43 No. 4, pp. 699-708.
-
(1992)
Computers & Structures
, vol.43
, Issue.4
, pp. 699-708
-
-
Butler, R.1
Williams, F.W.2
-
10
-
-
85002602944
-
Aeroelastic design optimization program"
-
Dodd, A.J., Kadrinka, K.E., Loikkanen, M.J., Rommel, B.A., Sikes, G.D., Strong, R.C. and Tzong, T.J. (1990), "Aeroelastic design optimization program". Journal of Aircraft, Vol. 27 No. 12, pp. 1028-36.
-
(1990)
Journal of Aircraft
, vol.27
, Issue.12
, pp. 1028-1036
-
-
Dodd, A.J.1
Kadrinka, K.E.2
Loikkanen, M.J.3
Rommel, B.A.4
Sikes, G.D.5
Strong, R.C.6
Tzong, T.J.7
-
11
-
-
0030676212
-
-
Kissimmee, FL
-
Edwards, D.A., Williams, F.W. and Kennedy, D. (1997), "Novel optimum cost design approach illustrated by the stiffened panel code VICONOPT", 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, FL, pp. 2952-62.
-
(1997)
Novel Optimum Cost Design Approach Illustrated by the Stiffened Panel Code VICONOPT", 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
, pp. 2952-2962
-
-
Edwards, D.A.1
Williams, F.W.2
Kennedy, D.3
-
12
-
-
0026835516
-
Stacking-sequence optimization for buckling of laminated plates by integer programming"
-
Haftka, R.T. and Walsh, J.L. (1992), "Stacking-sequence optimization for buckling of laminated plates by integer programming", AIM Journal. Vol. 30 No. 3, pp. 814-19.
-
(1992)
AIM Journal.
, vol.30
, Issue.3
, pp. 814-819
-
-
Haftka, R.T.1
Walsh, J.L.2
-
14
-
-
0031061903
-
Aeroelastic optimisation of composite wings using the dynamic stiffness method"
-
Lillico, M., Butler, R., Guo, S.J. and Banerjee, J.R. (1997), "Aeroelastic optimisation of composite wings using the dynamic stiffness method". The Aeronautical Journal, Vol. 101 No. 1002, pp. 77-86.
-
(1997)
The Aeronautical Journal
, vol.101
, Issue.1002
, pp. 77-86
-
-
Lillico, M.1
Butler, R.2
Guo, S.J.3
Banerjee, J.R.4
-
15
-
-
0028714062
-
-
Hilton Head, SC
-
Mabson, G.E., Flynn, B.W., Ilcewicz, L.B. and Grasser, D.L. (1994), "The use of COSTADE in developing composite commercial aircraft fuselage structures", 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Hilton Head, SC, pp. 1384-93.
-
(1994)
The Use of COSTADE in Developing Composite Commercial Aircraft Fuselage Structures", 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
, pp. 1384-1393
-
-
Mabson, G.E.1
Flynn, B.W.2
Ilcewicz, L.B.3
Grasser, D.L.4
-
18
-
-
0001694169
-
The limits of economy of material in frame structures"
-
Michell, A.G.M. (1904), "The limits of economy of material in frame structures". Philosophical Magazine, Series 6, Vol. 8 No. 47, pp. 589-95.
-
(1904)
Philosophical Magazine, Series 6
, vol.8
, Issue.47
, pp. 589-595
-
-
Michell, A.G.M.1
-
19
-
-
85034173590
-
-
November 1-4, Hilton Head, SC
-
Nagendra, S., Haftka, R.T. and Gurdal, Z. (1993), "PASCOG: a genetic algorithm based design procedure for stiffened composite panels under stability and strain constraints", 10th DOD/NASA/FAA Conference on Fibrous Composites in Structural Design, November 1-4, Hilton Head, SC, pp. 299-28.
-
(1993)
PASCOG: A Genetic Algorithm Based Design Procedure for Stiffened Composite Panels under Stability and Strain Constraints", 10th DOD/NASA/FAA Conference on Fibrous Composites in Structural Design
, pp. 299-328
-
-
Nagendra, S.1
Haftka, R.T.2
Gurdal, Z.3
-
20
-
-
85002719016
-
-
Neill, D.J., Johnson, E.H. and Canfield, R. (1990), "ASTROS - a multidisdplinary automated structural design Tool", Journal of Aircraft, Vol. 27 No. 12, pp. 1021-7.
-
(1990)
ASTROS - A Multidisdplinary Automated Structural Design Tool", Journal of Aircraft
, vol.27
, Issue.12
, pp. 1021-1027
-
-
Neill, D.J.1
Johnson, E.H.2
Canfield, R.3
-
21
-
-
0002207938
-
-
Springer-Verlag, Berlin
-
Powell, M.J.D. (1978), "A fast algorithm for nonlinearly constrained optimisation calculations", Proceedings of the 1977 Dundee Conference on Numerical Analysis, Lecture Notes in Mathematics, Vol. 630, Springer-Verlag, Berlin, pp. 144-57.
-
(1978)
A Fast Algorithm for Nonlinearly Constrained Optimisation Calculations", Proceedings of the 1977 Dundee Conference on Numerical Analysis, Lecture Notes in Mathematics
, vol.630
, pp. 144-157
-
-
Powell, M.J.D.1
-
22
-
-
84991104497
-
-
Panama City, FL
-
Rohl, P.J., Mavris, D.W. and Schrage, D.P. (1994), "A multilevel wing design procedure centred on the ASTROS structural optimization system", 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, pp.1377-87.
-
(1994)
A Multilevel Wing Design Procedure Centred on the ASTROS Structural Optimization System", 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
, pp. 1377-1387
-
-
Rohl, P.J.1
Mavris, D.W.2
Schrage, D.P.3
-
23
-
-
0002032407
-
-
ASCE, New York, NY
-
Schmit, L.A. (1960), "Structural design by systematic synthesis", Proceedings of the 2nd Conference on Electronic Computation, ASCE, New York, NY, pp. 105-22.
-
(1960)
Structural Design by Systematic Synthesis", Proceedings of the 2nd Conference on Electronic Computation
, pp. 105-122
-
-
Schmit, L.A.1
-
24
-
-
85003406325
-
-
Schmit, L.A. (1981), "Structural synthesis-its genesis and development", AIM Journal, 1981, Vol. 19 No. 10, pp. 1249-63.
-
(1981)
Structural Synthesis-its Genesis and Development", AIM Journal, 1981
, vol.19
, Issue.10
, pp. 1249-1263
-
-
Schmit, L.A.1
-
25
-
-
0022544782
-
-
Shirk, M.H, Hertz, T.J. and Weisshaar, T.A. (1986), "Aeroelastic tailoring-theory, practice, and promise", Journal of Aircraft, Vol. 23 No. 1, pp. 6-18.
-
(1986)
Aeroelastic Tailoring-theory, Practice, and Promise", Journal of Aircraft
, vol.23
, Issue.1
, pp. 6-18
-
-
Shirk, M.H.1
Hertz, T.J.2
Weisshaar, T.A.3
-
26
-
-
0343186315
-
-
Taylor, J.M. and Butler, R. (1997), "Optimum design and validation of flat composite beams subject to frequency constraints", AIAA Journal, Vol. 35 No. 3, pp. 540-5.
-
(1997)
Optimum Design and Validation of Flat Composite Beams Subject to Frequency Constraints", AIAA Journal
, vol.35
, Issue.3
, pp. 540-545
-
-
Taylor, J.M.1
Butler, R.2
-
27
-
-
8644259015
-
-
Rome
-
Taylor, J.M., Butler, R. and Harrison, C. (1997), "Optimisation of composite wind-tunnel wing models for frequency, flutter and divergence", CEAS International Forum on Aeroelasticity and Structural Dynamics, Rome, Vol. 3, pp. 49-56.
-
(1997)
Optimisation of Composite Wind-tunnel Wing Models for Frequency, Flutter and Divergence", CEAS International Forum on Aeroelasticity and Structural Dynamics
, vol.3
, pp. 49-56
-
-
Taylor, J.M.1
Butler, R.2
Harrison, C.3
-
28
-
-
34250076701
-
Multiparameter structural optimization using FEM and multi-point explicit approximations"
-
Toropov, V., Filatov, A.A. and Polynkin, A.A. (1993), "Multiparameter structural optimization using FEM and multi-point explicit approximations". Structural Optimization, Vol. 6, pp. 7-14.
-
(1993)
Structural Optimization
, vol.6
, pp. 7-14
-
-
Toropov, V.1
Filatov, A.A.2
Polynkin, A.A.3
-
29
-
-
0004081663
-
-
Colorado Springs, CO.
-
Vanderplaats Research & Development, Inc. (1995), DOT User Manual-Version 4.20, Colorado Springs, CO.
-
(1995)
DOT User Manual-Version 4.20
-
-
-
30
-
-
0017503106
-
-
Wilkinson, K., Markowitz, J., Lerner, L, George, D. and Batill, S.M. (1977), " Fastop: a flutter and strength optimization program for lifting-surface structures", Journal of Aircarft, Vol. 14 No. 6, pp. 581-7.
-
(1977)
Fastop: A Flutter and Strength Optimization Program for Lifting-surface Structures", Journal of Aircarft
, vol.14
, Issue.6
, pp. 581-587
-
-
Wilkinson, K.1
Markowitz, J.2
Lerner, L.3
George, D.4
Batill, S.M.5
-
31
-
-
0026253658
-
-
Williams, F.W., Kennedy, D., Butler, R. and Anderson, M.S. (1991), "VICONOPT: program for exact vibration and buckling analysis or design of prismatic plate assemblies", AIAA Journal, Vol. 29 No. 11, pp. 1927-8.
-
(1991)
VICONOPT: Program for Exact Vibration and Buckling Analysis or Design of Prismatic Plate Assemblies", AIAA Journal
, vol.29
, Issue.11
, pp. 1927-1928
-
-
Williams, F.W.1
Kennedy, D.2
Butler, R.3
Anderson, M.S.4
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