Response surface models combining linear and euler aerodynamics for supersonic transport design

Journal of Aircraft

Volumn 36, Issue 1, 1999, Pages 75-86

  Knill, Duane L ^a,b,c   Giunta, Anthony A ^a,b,d   Baker, Chuck A ^a,b   Grossman, Bernard ^a,b   Mason, William H ^a,b   Haftka, Raphael T ^a,b,e   Watson, Layne T ^a,b  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b Multidisc Anal/Des Ctr Adv V   (United States)

^c UNIVERSITY OF WASHINGTON   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

^e UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; EQUATIONS OF MOTION; MATHEMATICAL MODELS; OPTIMIZATION; PARALLEL PROCESSING SYSTEMS; SUPERSONIC AERODYNAMICS;

EULER EQUATION; HIGH SPEED CIVIL TRANSPORTS; RESPONSE SURFACES; VARIABLE COMPLEXITY MODELING;

TRANSPORT AIRCRAFT;

EID: 0032738174     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2415     Document Type: Article

References (10)

1. Giesing, J. P., Agrawal, S., and Bharadvaj, B. K., "The Role of Computational Fluid Dynamics in Multidisciplinary Design Optimization of Transport Aircraft," Proceedings of the 6th International Symposium on Computational Fluid Dynamics, Technology, and Operations Congress (Lake Tahoe, CA), 1995.
2. Nicolai, L. M., Fundamentals of Aircraft Design, E. P. Domicone Printing Services, Fairborne, OH, 1975, pp. 24·23-24·25.
3. Hutchison, M. G., Unger, E. R., Mason, W. H., Grossman, B., and Haftka, R. T., "Variable-Complexity Aerodynamic Optimization of a High-Speed Civil Transport Wing," Journal of Aircraft, Vol. 31, No. 1, 1994, pp. 110-116.
4. 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," AIAA Paper 95-1886, June 1995.
5. 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." Journal of Computational Mechanics, Vol. 18, No. 2, 1996, pp. 112-126.
6. Balabanov, V., Kaufman, M., Knill, D. L., Haim, D., Golovidov, O., Giunta, A. A., Haftka, R. T., Grossman, B., Mason, W. H., and Watson, L. T., "Dependence of Optimal Structural Weight on Aerodynamic Shape for a High-Speed Civil Transport," AIAA Paper 96-4046, Sept. 1996.
7. Burgee, S., Giunta, A. A., Balabanov, V., Grossman, B., Mason, W. H., Narducci, R., Haftka, R. T., and Watson, L. T., "A Coarse Grained Parallel Variable-Complexity Multidisciplinary Optimization Paradigm," International Journal of Supercomputing Applications and High Performance Computing, Vol. 10, No. 4, 1996, pp. 269-299.
8. Eminton, E., "On the Minimization and Numerical Evaluation of Wave Drag," Royal Aircraft Establishment, Rep. AERO.2564, Nov. 1955.
9. Harris, R. V., Jr., "An Analysis and Correlation of Aircraft Wave Drag," NASA TM X-947, March 1964.
10. Carlson, H. W., and Miller, D. S., "Numerical Methods for the Design and Analysis of Wings at Supersonic Speeds," NASA TN D-7713. Dec. 1974.