-
1
-
-
0003516505
-
-
AIAA, Washington, DC, Chaps. 5 and 6
-
Hoblit, F. M., Gust Loads on Aircraft: Concepts and Applications, AIAA, Washington, DC, 1988, Chaps. 5 and 6.
-
(1988)
Gust Loads on Aircraft: Concepts and Applications
-
-
Hoblit, F.M.1
-
2
-
-
0003586962
-
-
NASA TR-R-199, June
-
Houbolt, J. C., Steiner, R., and Pratt, K. G., "Dynamic Response of Airplanes to Atmospheric Turbulence Including Flight Data on Input and Response," NASA TR-R-199, June 1964.
-
(1964)
Dynamic Response of Airplanes to Atmospheric Turbulence Including Flight Data on Input and Response
-
-
Houbolt, J.C.1
Steiner, R.2
Pratt, K.G.3
-
3
-
-
0013160324
-
Handbook for Aeroelastic Analysis
-
MacNeal-Schwendler Corp., Los Angeles, CA, Nov.
-
"Handbook for Aeroelastic Analysis," MSC/NASTRAN Ver. 65, MacNeal-Schwendler Corp., Los Angeles, CA, Nov. 1987.
-
(1987)
MSC/NASTRAN Ver. 65
-
-
-
4
-
-
0005895530
-
-
Advisory Group for Aerospace Research and Development, AGARD-AG-317, Neuilly sur Seine, France, May
-
Manual on Flight of Flexible Aircraft in Turbulence, Advisory Group for Aerospace Research and Development, AGARD-AG-317, Neuilly sur Seine, France, May 1991.
-
(1991)
Manual on Flight of Flexible Aircraft in Turbulence
-
-
-
5
-
-
0032756411
-
Integrated Aeroservoelastic Optimization: Status and Direction
-
Livne, E., "Integrated Aeroservoelastic Optimization: Status and Direction," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 122-145.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 122-145
-
-
Livne, E.1
-
6
-
-
85002560541
-
Towards an Integrated Approach to the Optimum Design of Actively Controlled Composite Wings
-
Livne, E., Schmit, L. A., and Friedmann, P. P., "Towards an Integrated Approach to the Optimum Design of Actively Controlled Composite Wings," Journal of Aircraft, Vol. 27, No. 12, 1990, pp. 979-992.
-
(1990)
Journal of Aircraft
, vol.27
, Issue.12
, pp. 979-992
-
-
Livne, E.1
Schmit, L.A.2
Friedmann, P.P.3
-
7
-
-
0027593711
-
Integrated Structure/Control/Aerodynamic Synthesis of Actively Controlled Composite Wings
-
Livne, E., Schmit, L. A., and Friedmann, P. P., "Integrated Structure/Control/Aerodynamic Synthesis of Actively Controlled Composite Wings," Journal of Aircraft, Vol. 30, No. 3, 1993, pp. 387-394.
-
(1993)
Journal of Aircraft
, vol.30
, Issue.3
, pp. 387-394
-
-
Livne, E.1
Schmit, L.A.2
Friedmann, P.P.3
-
8
-
-
0032735199
-
Integrated Aeroservoelastic Optimization in the Design of Aerospace Systems
-
Bindolino, G., Ricci, S., and Mategazza, P., "Integrated Aeroservoelastic Optimization in the Design of Aerospace Systems," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 167-175.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 167-175
-
-
Bindolino, G.1
Ricci, S.2
Mategazza, P.3
-
9
-
-
0032715079
-
Reduced-Order Models for Integrated Aeroservoelastic Optimization
-
Karpel, M., "Reduced-Order Models for Integrated Aeroservoelastic Optimization," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 146-155.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 146-155
-
-
Karpel, M.1
-
10
-
-
0031140632
-
Modal-Based Structural Optimization with Static Aeroelastic and Stress Constraints
-
Karpel, M., Moulin, B., and Love, M. H., "Modal-Based Structural Optimization with Static Aeroelastic and Stress Constraints," Journal of Aircraft, Vol. 34, No. 3, 1997, pp. 433-440.
-
(1997)
Journal of Aircraft
, vol.34
, Issue.3
, pp. 433-440
-
-
Karpel, M.1
Moulin, B.2
Love, M.H.3
-
11
-
-
0032074002
-
Modal-Based Enhancement of Integrated Design Optimization Schemes
-
Karpel, M., "Modal-Based Enhancement of Integrated Design Optimization Schemes," Journal of Aircraft, Vol. 35, No. 3, 1998, pp. 437-444.
-
(1998)
Journal of Aircraft
, vol.35
, Issue.3
, pp. 437-444
-
-
Karpel, M.1
-
12
-
-
0032757435
-
Aeroelastic Loads and Sensitivity Analysis for Structural Loads Optimization
-
D'vari, R., and Baker, M., "Aeroelastic Loads and Sensitivity Analysis for Structural Loads Optimization," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 156-166.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 156-166
-
-
D'vari, R.1
Baker, M.2
-
13
-
-
0028498759
-
Continuous Gust Response and Sensitivity Derivatives Using State-Space Models
-
Zole, A., and Karpel, M., "Continuous Gust Response and Sensitivity Derivatives Using State-Space Models," Journal of Aircraft, Vol. 31, No. 5, 1994, pp. 1212-1214.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.5
, pp. 1212-1214
-
-
Zole, A.1
Karpel, M.2
-
14
-
-
0005849358
-
Aeroelastic Sensitivity Analyses for Flutter Speed and Gust Response
-
Balis Crema, L., Mastrodi, F., and Coppotelli, G., "Aeroelastic Sensitivity Analyses for Flutter Speed and Gust Response," Journal of Aircraft, Vol. 37, No. 1, 2000, pp. 172-180.
-
(2000)
Journal of Aircraft
, vol.37
, Issue.1
, pp. 172-180
-
-
Balis Crema, L.1
Mastrodi, F.2
Coppotelli, G.3
-
15
-
-
0004186280
-
-
Dover, New York
-
Bisplinghoff, R. L., and Ashley, H., Principles of Aeroelasticity, Dover, New York, 1975, pp. 350, 417.
-
(1975)
Principles of Aeroelasticity
, pp. 350
-
-
Bisplinghoff, R.L.1
Ashley, H.2
-
16
-
-
0004042750
-
-
Prentice-Hall, Upper Saddle River, NJ
-
Hurty, W. C., and Rubinstein, M. F., Dynamics of Structures, Prentice-Hall, Upper Saddle River, NJ, 1964, pp. 299-307.
-
(1964)
Dynamics of Structures
, pp. 299-307
-
-
Hurty, W.C.1
Rubinstein, M.F.2
-
18
-
-
0020814108
-
On the Application of the Mode-Acceleration Method to Structural Engineering Problems
-
Cornwell, R. E., Craig, R. R., Jr., and Johnson, C. P., "On the Application of the Mode-Acceleration Method to Structural Engineering Problems," Earthquake Engineering and Structural Dynamics, Vol. 11, No. 5, 1983, pp. 679-688.
-
(1983)
Earthquake Engineering and Structural Dynamics
, vol.11
, Issue.5
, pp. 679-688
-
-
Cornwell, R.E.1
Craig Jr., R.R.2
Johnson, C.P.3
-
19
-
-
0024732154
-
Calculation of Structural Dynamic Forces and Stresses Using Mode Acceleration
-
Blleloch, Paul, "Calculation of Structural Dynamic Forces and Stresses Using Mode Acceleration," AIAA Journal, Vol. 12, No. 5, 1988, pp. 760-762.
-
(1988)
AIAA Journal
, vol.12
, Issue.5
, pp. 760-762
-
-
Blleloch, P.1
-
20
-
-
0019009841
-
DYLOFLEX: A Computer Program for Flexible Aircraft Flight Dynamic Loads Analysis with Active Controls
-
20 Perry, B., III, Kroll, R. I., Miller, R. D., and Goetz, R. C., "DYLOFLEX: A Computer Program for Flexible Aircraft Flight Dynamic Loads Analysis with Active Controls," Journal of Aircraft, Vol. 17, No. 4, 1980, pp. 275-282.
-
(1980)
Journal of Aircraft
, vol.17
, Issue.4
, pp. 275-282
-
-
Perry III, B.1
Kroll, R.I.2
Miller, R.D.3
Goetz, R.C.4
-
21
-
-
0021788636
-
Dynamic Loads Analyses of Flexible Airplanes - New and Existing Techniques
-
Pototzky, A. S., and Perry, B., "Dynamic Loads Analyses of Flexible Airplanes - New and Existing Techniques," AIAA Paper 85-0808, 1985.
-
(1985)
AIAA Paper
, vol.85
, Issue.808
-
-
Pototzky, A.S.1
Perry, B.2
-
22
-
-
0021973369
-
Application of Ritz Vectors for Dynamic Analysis of Large Structures
-
Arnold, R. R., Citerley, R. L., Chargin, M., and Galant, D., "Application of Ritz Vectors for Dynamic Analysis of Large Structures," Computers and Structures, Vol. 21, No. 5, 1985, pp. 901-908; also Vol. 21, No. 3, 1985, pp. 461-467.
-
(1985)
Computers and Structures
, vol.21
, Issue.5
, pp. 901-908
-
-
Arnold, R.R.1
Citerley, R.L.2
Chargin, M.3
Galant, D.4
-
23
-
-
0021866187
-
-
Arnold, R. R., Citerley, R. L., Chargin, M., and Galant, D., "Application of Ritz Vectors for Dynamic Analysis of Large Structures," Computers and Structures, Vol. 21, No. 5, 1985, pp. 901-908; also Vol. 21, No. 3, 1985, pp. 461-467.
-
(1985)
Computers and Structures
, vol.21
, Issue.3
, pp. 461-467
-
-
-
24
-
-
0022889148
-
Dynamic Analysis Using a Reduced Basis of Exact Modes and Ritz Vectors
-
Kline, K. A., "Dynamic Analysis Using a Reduced Basis of Exact Modes and Ritz Vectors," AIAA Journal, Vol. 24, No. 12, 1986, pp. 2022-2029.
-
(1986)
AIAA Journal
, vol.24
, Issue.12
, pp. 2022-2029
-
-
Kline, K.A.1
-
25
-
-
0029777766
-
The Fictitious Mass Element in Structural Dynamics
-
Karpel, M., and Raveh, D., "The Fictitious Mass Element in Structural Dynamics," AIAA Journal, Vol. 34, No. 3, 1996, pp. 607-613.
-
(1996)
AIAA Journal
, vol.34
, Issue.3
, pp. 607-613
-
-
Karpel, M.1
Raveh, D.2
-
26
-
-
0034188622
-
Reduced Order Design-Oriented Stress Analysis Using Combined Direct and Adjoint Solutions
-
Livne, E., and Blando, G. D., "Reduced Order Design-Oriented Stress Analysis Using Combined Direct and Adjoint Solutions," AIAA Journal, Vol. 38, No. 5, 2000, pp. 898-909.
-
(2000)
AIAA Journal
, vol.38
, Issue.5
, pp. 898-909
-
-
Livne, E.1
Blando, G.D.2
-
27
-
-
0042813601
-
Structural Dynamic Frequency Response Using Combined Direct and Adjoint Reduced-Order Approximations
-
Livne, E., and Blando, G. D., "Structural Dynamic Frequency Response Using Combined Direct and Adjoint Reduced-Order Approximations," AIAA Journal, Vol. 41, No. 7, 2003, pp. 1377-1385.
-
(2003)
AIAA Journal
, vol.41
, Issue.7
, pp. 1377-1385
-
-
Livne, E.1
Blando, G.D.2
-
28
-
-
0003507691
-
-
Ginn and Co., Waltham, MA, Chap. 10 and 11
-
Bryson, A. E., and Ho, Y-C., Applied Optimal Control, Ginn and Co., Waltham, MA, 1969, Chap. 10 and 11.
-
(1969)
Applied Optimal Control
-
-
Bryson, A.E.1
Ho, Y.-C.2
-
29
-
-
0005845915
-
-
NASA TP-1876, Aug.
-
Mukhopadhyay, V., Newsome, J. R., and Abel, I., "A Method for Obtaining Reduced-Order Control Laws for High Order Systems Using Optimization Techniques," NASA TP-1876, Aug. 1981.
-
(1981)
A Method for Obtaining Reduced-order Control Laws for High Order Systems Using Optimization Techniques
-
-
Mukhopadhyay, V.1
Newsome, J.R.2
Abel, I.3
-
30
-
-
0027611019
-
Alternative Approximations for Integrated Control/Structure Aeroservoelastic Synthesis
-
Livne, E., "Alternative Approximations for Integrated Control/Structure Aeroservoelastic Synthesis," AIAA Journal, Vol. 31, No. 6, 1993, pp. 1100-1108.
-
(1993)
AIAA Journal
, vol.31
, Issue.6
, pp. 1100-1108
-
-
Livne, E.1
-
31
-
-
0021654639
-
Structural Optimization - Some Key Ideas and Insights
-
edited by E. Atrek, R. H. Gallagher, K. M. Ragsdell, and O. C. Zienkiewicz, Wiley, New York
-
Schmit, L. A., "Structural Optimization - Some Key Ideas and Insights," New Directions in Optimum Structural Design, edited by E. Atrek, R. H. Gallagher, K. M. Ragsdell, and O. C. Zienkiewicz, Wiley, New York, 1984.
-
(1984)
New Directions in Optimum Structural Design
-
-
Schmit, L.A.1
-
32
-
-
0004095331
-
-
Kluwer Academic, Norwell, MA, Chap. 6
-
Haftka, R. T., and Gurdal, Z., Elements of Structural Optimization, 3rd ed., Kluwer Academic, Norwell, MA, 1992, Chap. 6.
-
(1992)
Elements of Structural Optimization, 3rd Ed.
-
-
Haftka, R.T.1
Gurdal, Z.2
-
33
-
-
0003253733
-
Equivalent Plate Modeling for Conceptual Design of Aircraft Wing Structures
-
Sept.
-
Giles, G. L., "Equivalent Plate Modeling for Conceptual Design of Aircraft Wing Structures," AIAA Paper 95-3945, Sept. 1995.
-
(1995)
AIAA Paper
, vol.95
, Issue.3945
-
-
Giles, G.L.1
-
34
-
-
0032759298
-
Design Oriented Analysis of Fuselage Structures Using Equivalent Plate Methodology
-
Giles, G. L., "Design Oriented Analysis of Fuselage Structures Using Equivalent Plate Methodology," Journal of Aircraft, Vol. 36, No. 1, 1999, pp. 21-28.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 21-28
-
-
Giles, G.L.1
-
35
-
-
0028466515
-
Lessons from Application of Equivalent Plate Structural Modeling to an HSCT Wing
-
Livne, E., Sels, R. A., and Bhatia, K. G., "Lessons from Application of Equivalent Plate Structural Modeling to an HSCT Wing," Journal of Aircraft, Vol. 31, No. 4, 1994, pp. 953-960.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.4
, pp. 953-960
-
-
Livne, E.1
Sels, R.A.2
Bhatia, K.G.3
-
36
-
-
84888983941
-
Evaluation of Equivalent Laminated Plate Solution (ELAPS) in HSCT Sizing
-
April
-
Stone, S. C., Henderson, J. L., Nazari, M. M., Boyd, W. N., Becker, B. T., Bhatia, K. G., Giles, G. L., and Wrenn, G. A., "Evaluation of Equivalent Laminated Plate Solution (ELAPS) in HSCT Sizing," AIAA Paper 2000-1452, April 2000.
-
(2000)
AIAA Paper
, vol.2000
, Issue.1452
-
-
Stone, S.C.1
Henderson, J.L.2
Nazari, M.M.3
Boyd, W.N.4
Becker, B.T.5
Bhatia, K.G.6
Giles, G.L.7
Wrenn, G.A.8
-
37
-
-
0028447366
-
Equivalent Plate Structural Modeling for Wing Shape Optimization Including Transverse Shear
-
Livne, E., "Equivalent Plate Structural Modeling for Wing Shape Optimization Including Transverse Shear," AIAA Journal, Vol. 32, No. 6, 1994, pp. 1278-1288.
-
(1994)
AIAA Journal
, vol.32
, Issue.6
, pp. 1278-1288
-
-
Livne, E.1
-
38
-
-
0004024952
-
-
Ph.D. Dissertation, Dept. of Mechanical, Aerospace, and Nuclear Engineering, Univ. of California, Los Angeles, Sept.
-
Livne, E., "Integrated Multidisciplinary Optimization of Actively Controlled Fiber Composite Wings," Ph.D. Dissertation, Dept. of Mechanical, Aerospace, and Nuclear Engineering, Univ. of California, Los Angeles, Sept. 1990.
-
(1990)
Integrated Multidisciplinary Optimization of Actively Controlled Fiber Composite Wings
-
-
Livne, E.1
-
39
-
-
0017685541
-
Airplane Math Modeling Methods for Active Control Design
-
Structural Aspects of Active Controls, AGARD-CP-228, Lissabon, Portugal, April
-
Roger, K. L., "Airplane Math Modeling Methods for Active Control Design," Proceedings of the 44th AGARD Structures and Material Panel, Structural Aspects of Active Controls, AGARD-CP-228, Lissabon, Portugal, April 1977, pp. 4.1-4.11.
-
(1977)
Proceedings of the 44th AGARD Structures and Material Panel
-
-
Roger, K.L.1
-
40
-
-
0025207009
-
Time Domain Aeroservoelastic Modeling Using Weighted Unsteady Aerodynamic Forces
-
Karpel, M., "Time Domain Aeroservoelastic Modeling Using Weighted Unsteady Aerodynamic Forces," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 1, 1990, pp. 30-37.
-
(1990)
Journal of Guidance, Control, and Dynamics
, vol.13
, Issue.1
, pp. 30-37
-
-
Karpel, M.1
-
41
-
-
0022506342
-
Monte Carlo Turbulence Simulation Using Rational Approximations to Von Karman Spectra
-
Campbell, C. W., "Monte Carlo Turbulence Simulation Using Rational Approximations to Von Karman Spectra," AIAA Journal, Vol. 24, No. 1, 1986, pp. 62-66.
-
(1986)
AIAA Journal
, vol.24
, Issue.1
, pp. 62-66
-
-
Campbell, C.W.1
-
42
-
-
0016971709
-
Repetitive Flutter Calculations in Structural Design
-
Haftka, R. T., and Yates, E. C., "Repetitive Flutter Calculations in Structural Design," Journal of Aircraft, Vol. 13, No. 7, 1976, pp. 454-461.
-
(1976)
Journal of Aircraft
, vol.13
, Issue.7
, pp. 454-461
-
-
Haftka, R.T.1
Yates, E.C.2
-
43
-
-
0003204675
-
Aeroelastic Analysis Using Finite Element Models
-
DGLR/AAAF/RAES, Aachen, Germany, April
-
Nicot, P., and Petiau, C., "Aeroelastic Analysis Using Finite Element Models," DGLR/AAAF/RAES, European Forum on Aeroelasticity and Structural Dynamics, Aachen, Germany, April 1989.
-
(1989)
European Forum on Aeroelasticity and Structural Dynamics
-
-
Nicot, P.1
Petiau, C.2
-
44
-
-
0025448044
-
High Quality Approximation of Eigenvalues in Structural Optimization
-
Canfield, R. A., "High Quality Approximation of Eigenvalues in Structural Optimization," AIAA Journal, Vol. 28, No. 6, 1990, pp. 1116-1122.
-
(1990)
AIAA Journal
, vol.28
, Issue.6
, pp. 1116-1122
-
-
Canfield, R.A.1
-
45
-
-
0027608488
-
Design of Frames Against Buckling Using a Rayleigh Quotient Approximation
-
Canfield, R. A., "Design of Frames Against Buckling Using a Rayleigh Quotient Approximation," AIAA Journal, Vol. 31, No. 6, 1993, pp. 1143-1149.
-
(1993)
AIAA Journal
, vol.31
, Issue.6
, pp. 1143-1149
-
-
Canfield, R.A.1
-
46
-
-
0005845918
-
Design-Oriented Quadratic Stress Failure Constraints for Actively Controlled Structures under Combined Steady and Random Excitation
-
to be published
-
Engelsen, F., and Livne, E., "Design-Oriented Quadratic Stress Failure Constraints for Actively Controlled Structures under Combined Steady and Random Excitation," AIAA Journal (to be published).
-
AIAA Journal
-
-
Engelsen, F.1
Livne, E.2
-
47
-
-
0003965075
-
-
Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Univ. of Washington, Seattle, Aug.
-
Engelsen, F., "Design-Oriented Gust Stress Constraints for Aeroservoelastic Design Synthesis," Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Univ. of Washington, Seattle, Aug. 2001.
-
(2001)
Design-oriented Gust Stress Constraints for Aeroservoelastic Design Synthesis
-
-
Engelsen, F.1
-
48
-
-
0028392753
-
Modal Coordinates for Aeroelastic Analysis with Large Local Structural Variations
-
Karpel, M., and Wieseman, C. D., "Modal Coordinates for Aeroelastic Analysis with Large Local Structural Variations," Journal of Aircraft, Vol. 31, No. 2, 1994, pp. 396-403.
-
(1994)
Journal of Aircraft
, vol.31
, Issue.2
, pp. 396-403
-
-
Karpel, M.1
Wieseman, C.D.2
|