Computational fluid dynamics for aerodynamic design: Its current and future impact

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Jameson, Antony ^a   Vassberg, John C ^b  

^a 496 Lomita Mall   (United States)

^b BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; APPLICATION PROGRAMS; COMPUTATIONAL FLUID DYNAMICS; COST FUNCTIONS; DESIGN; ECONOMIC AND SOCIAL EFFECTS; SHAPE OPTIMIZATION;

AERODYNAMIC DESIGNS; AERODYNAMIC OPTIMIZATION; AERODYNAMIC SHAPE OPTIMIZATION; AIRCRAFT DEVELOPMENT; COMPUTATIONAL COSTS; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; COMPUTER EQUIPMENTS; OPTIMIZATION METHOD;

AERODYNAMICS;

EID: 85085404450     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-538     Document Type: Conference Paper

References (17)

1. M. Van Dyke. An Album of Fluid Motion. The Parabolic Press, Stanford, 1982.
2. R. M. Hicks and P. A. Henne. Wing design by numerical optimization. Journal of Aircraft, 15:407-412, 1978.
3. C. Bischof, A. Carle, G. Corliss, A. Griewank, and P. Hovland. Generating derivative codes from Fortran programs. Internal report MCSP263-0991, Computer Science Division, Argonne National Lab. and Center of Research on Parallel Computation, Rice Univ., 1991.
4. L. L. Green, P. A. Newman, and K. J. Haigler. Sensitivity derivatives for advanced CFD algorithm and viscous modeling parameters via automatic differentiation. AIAA paper 93-3321, llth AIAA Computational Fluid Dynamics Conference, Orlando, Florida, 1993.
5. W. K. Anderson, J. C. Newman, D. L. Whitfield, and E. J. Nielsen. Sensitivity analysis for the Navier-Stokes equations on unstructured meshes using complex variables. AIAA paper 99-3294, Norfolk, VA, June 1999.
6. A. Jameson, L. Martinelli, J. J. Alonso, J. C. Vassberg, and J. Reuther. Simulation based aerodynamic design. IEEE Aerospace Conference, Big Sky, MO, March 2000.
7. A. Jameson. Optimum aerodynamic design using control theory. Computational Fluid Dynamics Review, pages 495-528, 1995.
8. A. Jameson. Optimum aerodynamic design using CFD and control theory. AIAA paper 95-1729, AIAA 12th Computational Fluid Dynamics Conference, San Diego, CA, June 1995.
9. A. Carle, M. Pagan, and L. L. Green. Preliminary results from the application of automated adjoint code generation to CFL3D. AIAA paper 98-4807, 1998.
10. A. Jameson and J. C. Vassberg. Studies of alternative numerical optimization methods applied to the brachistochrone problem. In Proceedings of OptiCON'99, Newport Beach, CA, October 1999.
11. P. E. Gill, W. Murray, M. A. Saunders, and M. H. Wright. User's guide for npsol (version 4.0): A fortran package for nonlinear programming. Technical Report SOL 86-2, Department of Operations Research, Stanford University, Jan. 1986.
12. A. Jameson. Aerodynamic design via control theory. Journal of Scientific Computing, 3:233-260, 1988.
13. E. Ahlstrom, R. Gregg, J. Vassberg, and A. Jameson. G-Force: The design of an unlimited class Reno racer. AIAA paper 2000-4341, 18th AIAA Applied Aerodynamics Conference, Denver, CO, August 2000.
14. J. Gallman, J. Reuther, N. Pfeiffer, W. Forrest, and D. Bernstorf. Business jet wing design using aerodynamic shape optimization. AIAA paper 96-0554, 34th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 1996.
15. J. Reuther, J.J. Alonso, M.J. Rimlinger, and A. Jameson. Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on parallel computers. AIAA paper 96-4045, 6th AIAA/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Bellevue, WA, September 1996.
16. J. J. Reuther, A. Jameson, J. J. Alonso, M. Rimlinger, and D. Saunders. Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers: Part i. Journal of Aircraft, 36:51-60, 1998.
17. J. J. Reuther, A. Jameson, J. J. Alonso, M. Rimlinger, and D. Saunders. Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computers: Part ii. Journal of Aircraft, 36:61-74, 1998.