• Kaufman, M., Balabanov, V., Burgee, S., Giunta, A. A., Grossman, B., Mason, W. H., Watson, L. T., and Haftka, R. T., “Variable Complexity Response Surface Approximations For Wing Structural Weight,” AIAA 34th Aerospace Sciences Meeting and Exhibit, AIAA Paper 96-0089, Jan., 1996.

• Knill, D. L., Grossman, B., Mason, W. H., and Haftka, R. T., “Certification of an Euler code for High-Speed Civil Transport Optimization,” AIAA 34th Aerospace Sciences Meeting and Exhibit, AIAA Paper 96-0330, Jan., 1996.

• Lutze, F.H., Durham, W.C., and Mason, W.H., “Unified Development of Lateral-Directional Departure Criteria,” Journal of Guidance, Control and Dyn., Vol. 19, No. 2, March-April 1996, pp. 489-493.

• Malone, B., and Mason, W.H., “Aircraft Concept Optimization Using Parametric Multiobjective Figures of Merit,” Journal of Aircraft, Vol. 33, No. 2, March-April 1996, pp. 444-445.

• Balabanov, V, Kaufman, M.., Giunta, A.A., Haftka, R.T., Grossman, B., Mason, W.H., and Watson, L.T., “Developing Customized Wing Weight Function by Structural Optimization on Parallel Computers,” AIAA Paper 96-1336, Proceedings of the 37th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, Salt Lake City, UT, April 15-17, 1996, pp. 113-125.
  

• Huang, X., Dudley, J., Haftka, R. T., Grossman, and Mason, W.H., “Structural Weight Estimation for Multidisciplinary Optimization of a High-Speed Civil Transport,” Journal of Aircraft, Vol. 33, No. 3, May - June 1996, pp. 608-616

• Kaufman, M., Balabanov, V., Burgee, S.L., Giunta, A.A., Grossman, B., Haftka, R.T., Mason, W.H., and Watson, L.T., “Variable-complexity response surface approximations for wing structural weight in HSCT design,” Computational Mechanics, Vol. 18, No. 2, June 1996, pp. 112-126.

• Balabanov, V, Giunta, A.A., Grossman, B., Mason, W.H., Watson, L.T.and Haftka, R.T., “Parallel Computing and Variable-Complexity Modeling Strategies for HSCT Design,” NASA Computational Aerosciences Workshop, NASA Ames Research Center, August 13-15, 1996.
  

• Giunta, A.A., Balabanov, V., Haim, D., Grossman, B., Mason, W.H., Watson, L.T, and Haftka, R.T., “Wing Design for a High-Speed Civil Transport Using a Design of Experiments Methodology,” AIAA Paper 96-4001, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Sept. 1996. pp. 168-183.

• Chai, S., and Mason, W.H., “Landing Gear Integration in Aircraft Conceptual Design,” AIAA Paper 96-4038, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Sept. 1996. pp. 525-540.

• Balabanov, V, Kaufman, M., Knill, D.L., Giunta, A.A., Haftka, R.T., Grossman, B., Mason, W.H., and Watson, L.T., “Dependence of Optimum Structural Weight on Aerodynamic Shape for a High-Speed Civil Transport,” AIAA 96-4046, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Sept. 1996. pp. 599-612. NOTE: This paper was chosen as the recipient of the 6th Symposium on Mutidisciplinary Analysis and Optimization Best Paper Award.

• Anderson, M. A., and Mason, W.H., “An MDO Approach to Control-Configured-Vehicle Design,” AIAA Paper 96-4058, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, Sept. 1996. pp. 734-743.

• Crisafulli, P.J., Kaufman, M., Giunta, A.A., Mason, W.H., Grossman, B., Watson, L.T, and Haftka, R.T, “Response Surface Approximations for Pitching Moment, Including Pitch-Up, in the MDO Design of an HSCT”, AIAA Paper 96-4136, Proceedings of the 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Sept. 1996. pp. 1308-1322.

• Burgee, S., Giunta, A.A., Balabanov, V., Grossman, B., Mason, W. H., Narducci, R., Haftka, R. T., and Watson, L. T., “A Coarse Grained Variable-Complexity Multidisciplinary Optimization Paradigm,” Intl. J. Supercomputing Applications and High Performance Computing, Vol. 10, No. 4, 1996, pp. 269-299.

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