Aerodynamic shape optimization of wing and wing-body configurations using control theory

33rd Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1995, Pages

  Reuther, J ^a   Jameson, A ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b PRINCETON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AEROSPACE ENGINEERING; CONTROL THEORY; MAPPING; MESH GENERATION; SWEPT WINGS;

AERODYNAMIC SHAPE OPTIMIZATION; BODY DESIGN; FITTED MESH; MAPPING FUNCTIONS; OPTIMIZATION PROCEDURES; OPTIMIZATION TECHNIQUES; WING-BODY CONFIGURATIONS;

SHAPE OPTIMIZATION;

EID: 0041516133     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1995-123     Document Type: Conference Paper

References (37)

1. F. Bauer, P. Garabedian, D. Korn, and A. Jameson. Supercritical Wing Sections 2. Springer Verlag, New York, 1975.
2. O. Baysal and M. E. Eleshaky. Aerodynamic design optimization using sensitivity anaysis and computational fluid dynamics. AIAA paper 91-0471, 29th Aerospace Sciences Meeting, Reno, Nevada, January 1991.
3. O. Baysal and M. E. Eleshaky. Aerodynamic sensativity analysis methods for the compressible Euler equations. Journal of Fluids Engineering, 113(4):681-688, 1991.
4. O. Baysal and M. E. Eleshaky. Aerodynamic design optimization using sensitivity anaysis and computational fluid dynamics. AIAA Journal, 3Q(3):718-725,1992.
5. O. Baysal and M. E. Eleshaky. Airfoil shape optimization using sensitivity analysis on viscous flow equations. Journal of Fluids Engineering, 115:75-84, 1993.
6. G. W. Burgreen and O. Baysal. Aerodynamic shape optimization using preconditioned conjugate gradient methods. AIAA paper 93-3322, July 1993.
7. G. W. Burgreen and O. Baysal. Three-dimensional aerodynamic shape optimization of wings using sensitivity analysis. AIAA paper 94-0094, 32th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 1994.
8. M. E. Eleshaky and O. Baysal. Preconditioned domain decomposition scheme for three-dimensional aerodynamic sensitivity analysis. In Proceedings of of the 12th AIAA computational fluid dynamics conference, 10551056, July 1993.
9. M. E. Eleshaky and O. Baysal. Shape optimization of a 3-d nacelle near a flat plate wing using multiblock sensitivity analysis. AIAA paper 94-0160, 32th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 1994.
10. P.E. Gill, W. Murray, and M.H. Wright. Practical Optimization. Academic Press, 1981.
11. R. M. Hicks and P. A. Henne. Wing design by numerical optimization. Journal of Aircraft, 15:407-412, 1978.
12. R. M. Hicks and P. A. Henne. Wing design by numerical optimization. AIAA paper 79-0080, 1979.
13. R. M. Hicks, E. M. Murman, and G. N. Van-derplaats. An assessment of aifoil design by numerical optimization. NASA TMX-3092, Ames Research Center, Moffett Field, California, July 1974.
14. W.P. Huffman, R.G. Melvin, D.P. Young, F.T. Johnson, J.E. Bussoletti, M.B. Bieterman, and C.L. Hilmes. Practical design and optimization in computational fluid dynamics. AIAA paper 93-3111, AIAA 24th Fluid Dynamics Conference, Orlando, Florida, July 1993.
15. A. C. Taylor III, G. W. Hou, and V. M. Korivi. Sensitivity analysis, approximate anaysis, and design optimization for internal and external viscous flows. AIAA paper 91-3083, September 1991.
16. A. Jameson. Solution of the Euler equations for two dimensional transonic flow by a multigrid method. Applied Mathematics and Computations, 13:327-356, 1983.
17. A. Jameson. Multigrid algorithms for compressible flow calculations. In W. Hackbusch and U. Trottenberg, editors. Lecture Notes in Mathematics, Vol, 1228, 166-201. Proceedings of the 2nd European Conference on Multigrid Methods, Cologne, 1985, Springer-Verlag, 1986.
18. A. Jameson. Aerodynamic design via control theory. Journal of Scientific Computing, 3:233260, 1988.
19. A. Jameson. Automatic design of transonic airfoils to reduce the shock induced pressure drag. In Proceedings of the 31st Israel Annual Conference on Aviation and Aeronautics, Tel Aviv, 5-17, February 1990.
20. A. Jameson. Artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence in transonic and hypersonic flows. AIAA paper 93-3359, AIAA 11th Computational Fluid Dynamics Conference, Orlando, Florida, July 1993.
21. A. Jameson. Aerodynamic design methods. In International Workshop on Solution Techniques for Large-Scale CFD Problems, Montreal, September 1994. CERCA.
22. A. Jameson. Optimum aerodynamic design via boundary control. In AGARD-VKI Lecture Series, Optimum Design Methods in Aerodynamics, von Karman Institute for Fluid Dynamics, 1994.
23. A. Jameson and J. Reuther. Control theory based airfoil design using the Eu-ler equations. AIAA paper 91-4272, 5th AIAA/USAF/NASA/ISSMO Symposium on Muitidisciplinary Analysis and Optimization, Panama City Beach, FL, September 1993
24. V. M. Korivi, A. C. Taylor III, G. W. Hou, P. A. Newman, and H. E. Jones. Sensitivity derivatives for three-dimensional supersonic Euler code using incremental iterative strategy. In Proceedings of of the 12th AIAA computational fluid dynamics conference, 1053-1054, July 1993.
25. V. M. Korivi, A. C. Taylor III, and P. A. Newman. Aerodynamic optimization studies using a 3-d supersonic Euler code with efficient calculation of sensitivity derivatives. AIAA paper 94-4270, 5th AIAA/USAF/NASA/ISSMO Symposium on Muitidisciplinary Analysis and Optimization, Panama City, Florida, September 1994.
26. V. M. Korivi, A. C. Taylor III, P. A. Newman, G. W. Hou, and H. E. Jones. An incremental strategy for calculating consistent discrete CFD sensitivity derivatives. NASA TM 104207, Lan-gley Research Center, Hampton, VA, February 1992.
27. G. Kuruvila, S. Ta'Asan, and M. D. Salas. Airfoil optimization by the one-shot method. In AGARD-VKI Lecture Series, Optimum Design Methods in Aerodynamics, von Karman Institute for Fluid Dynamics, 1994.
28. J.M. Lacasse and O. Baysal. Design optimization of single- and two-element airfoils on multiblock grids. AIAA paper 94-4273, 5th AIAA/USAF/NASA/ISSMO Symposium on Muitidisciplinary Analysis and Optimization, Panama City, Florida, September 1994.
29. J. L. Lions. Optimal Control of Systems Governed by Pariial Differential Equations. Springer-Verlag, New York, 1971. Translated by S.K. Mitter.
30. P. A. Newman, G. W. Hou, H. E. Jones, A. C. Taylor III, and V. M. Korivi. Observations on computational methodologies for use in large-scale gradient-based, muitidisciplinary design incorporating advanced CFD codes. NASA TM 104206, Langley Research Center, Hampton, VA, February 1992.
31. O. Pironneau. Optimal Shape Design for Elliptic Systems. Springer-Verlag, New York, 1984.
32. O. Pironneau. Optimal shape design for aerodynamics. In AGARD-VKI Lecture Series, Optimum Design Methods in Aerodynamics, von Karman Institute for Fluid Dynamics, 1994.
33. J. Reuther, S. Cliff, R. Hicks, and C P. van Dam. Practical design optimization of wing/body configurations using the Euler equations. AIAA paper 92-2633, 1992.
34. J. Reuther and A. Jameson. Control theory based airfoil design for potential flow and a finite volume discretization. AIAA paper 91-499, 32th Aerospace Sciences Meeting and Exibit, Reno, Nevada, January 1994.
35. J. Reuther, CP. van Dam, and R. Hicks. Subsonic and transonic low-Reynolds-number airfoils with reduced pitching moments. Journal of Aircraft, 29:297-298, 1992.
36. S. Ta'asan, G. Kuruvila, and M D. Salas. Aerodynamic design and optimization in one shot. AIAA paper 91-005, 30th Aerospace Sciences Meeting and Exibit, Reno, Nevada, January 1992.
37. D.P. Young, W.P. Huffman, R.G. Melvin, M.B. Bieterman, C.L. Hilmes, and F.T. Johnson. Inexactness and global convergence in design optimization. AIAA paper 94-4286, 5th AIAA/USAF/NASA/ISSMO Symposium on Muitidisciplinary Analysis and Optimization, Panama City, Florida, September 1994.