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1
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0004505080
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Aircraft Configuration Op-timization Including Optimized Flight Profiles
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0028257638
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Variable- Complexity Aerodynamic Optimization of an HSCT Wing Using Structural Wing-Weight Equations
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Hutchison, M. G., Unger, E. R., Mason, W. H., Grossman, B., and Haftka, R. T., “Variable- Complexity Aerodynamic Optimization of an HSCT Wing Using Structural Wing-Weight Equations,” Journal of Aircraft, Vol. 31, No. 1, 1994, pp. 110-116.
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Hutchison, M.G.1
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AIAA Paper 94-4377
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Dudley, J., Huang, X., Haftka, R. T., Grossman, B., and Mason, W. H., “Variable-Complcxity Interlacing of Weight Equation and Structural Optimization for the Design of the High Speed Civil Transport,” AIAA Paper 94-4377, 1994.
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Variable-Complcxity Interlacing of Weight Equation and Structural Optimization for the Design of the High Speed Civil Transport
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Dudley, J.1
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0004623052
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Variable-Complexity Response Surface Approximations for Wing Structural Weight in HSCT Design
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AIAA Paper 96-0089, Reno, NV, Jan
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34Th Aerospace Sciences Meeting and Exhibit
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Kaufman, M.1
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Variable-Complexity Response Surface Aerodynamic Design of an HSCT Wing
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Giunta, A. A., Narducci, R., Burgee, S., Grossman, B., Mason, W. H., Watson, L. T., and Haftka, R. T., “Variable-Complexity Response Surface Aerodynamic Design of an HSCT Wing,” Proceedings of the 13th AIAA Applied Aerodynamics Conference, AIAA Paper 95-1886, pp. 994-1002, San Diego, CA, June 19-22, 1995.
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84978090917
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Pitch-up Characteristics for HSCT Class Planforms: Survey and Estimation
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AIAA Paper 94-1819, Colorado Springs, CO, June
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AIAA 12Th Applied Aerodynamics Conference
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MAD Center Report 96-07-01, July, Virginia Tech, Blacksburg, VA
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Trim, Control, and Performance Effects in Variable-Complexity High-Speed Civil Transport Design
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0022028013
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NEWSUMT-A: A General Purpose Program for Constrained Optimization Using Approximations
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Grandhi, R.V.1
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PhD Thesis, Virginia Polytechnic Institute & State University, Blacksburg, Virginia, Mar
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Hutchison, M. G., Multidisciplinary Optimization of High-Speed Civil Transport Configurations Using Variable-Complexity Modeling. PhD Thesis, Virginia Polytechnic Institute & State University, Blacksburg, Virginia, Mar. 1993.
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USAF Stability and Control DATCOM
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Arrow Wings for Supersonic Cruise Aircraft
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Factorial Designs, the | XTX | Criterion, and Some Related Matters
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Noisy Aerodynamic Response and Smooth Approximations in HSCT Design
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AIAA Paper 94-4376, Panama City Beach, FL, Sept
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Giunta, A. A., Dudley, J. M., Narducci, R., Grossman, B., Haftka, R. T., Mason, W. H., and Watson, L. T., “Noisy Aerodynamic Response and Smooth Approximations in HSCT Design,” Proceedings of the 5th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, AIAA Paper 94-4376, Panama City Beach, FL, Sept. 1994, pp. 1117-1128.
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