Aerodynamic optimization using sensitivity derivatives from a three-dimensional supersonic Euler code

Journal of Aircraft

Volumn 35, Issue 3, 1998, Pages 405-411

  Korivi, Vamshi Mohan ^a,c,d   Newman, Perry A ^b,e   Taylor III, Arthur C ^a,c,f  

^a OLD DOMINION UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Mechanical Engineering Department   (United States)

^d Optimal CAE Inc   (United States)

^e Fluid Mechanics and Acoustic Div   (United States)

^f AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; EQUATIONS OF MOTION; ITERATIVE METHODS; OPTIMIZATION; SENSITIVITY ANALYSIS; SUPERSONIC AERODYNAMICS; WINGS;

AERODYNAMIC SENSITIVITY DERIVATIVES; EULER EQUATIONS;

FLIGHT DYNAMICS;

EID: 0032072174     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2338     Document Type: Article

References (21)

1. Korivi, V. M., Taylor, A. C., III, Newman, P. A., Hou, G. J.-W., and Jones, H. E., "An Approximately-Factored Incremental Strategy for Calculating Consistent Discrete Aerodynamic Sensitivity Derivatives," Journal of Computational Physics, Vol. 113, No. 2, 1994, pp. 336-346; also AIAA Paper 92-4746, Sept. 1992.
2. Newman, P. A., Hou, G. J.-W., Jones, H. E., Taylor, A. C. III, and Korivi, V. M., "Observations on Computational Methodologies for Use in Large-Scale Gradient-Based Multidisciplinary Design," AIAA/ USAF/NASA/OAI 4th Symposium on Multidisciplinary Analysis and Optimization, Pt. 1, AIAA, Washington, DC, 1992, pp. 531-542.
3. Korivi, V. M., Taylor, A. C., III, Hou, G. J.-W., Newman, P. A., and Jones, H. E., "Sensitivity Derivatives for Three-Dimensional Supersonic Euler Code Using Incremental Iterative Strategy," AIAA 11th Computational Fluid Dynamics Conference, Pt. 2, AIAA, Washington, DC, 1993, pp. 1053, 1054; also AIAA Journal, Vol. 32, No. 6, 1994, pp. 1319-1321.
4. Korivi, V. M., Taylor, A. C., III, Hou, G. J.-W., Newman, P. A., and Jones, H. E., "Sensitivity Derivatives for Three-Dimensional Supersonic Euler Code Using Incremental Iterative Strategy," AIAA 11th Computational Fluid Dynamics Conference, Pt. 2, AIAA, Washington, DC, 1993, pp. 1053, 1054; also AIAA Journal, Vol. 32, No. 6, 1994, pp. 1319-1321.
5. Korivi, V. M., Newman, P. A., and Taylor, A. C., III, "Aerodynamic Optimization Studies Using a 3-D Supersonic Euler Code with Efficient Calculation of Sensitivity Derivatives," AIAA/USAF/NASA/ ISSMO 5th Symposium on Multidisciplinary Analysis and Optimization, Pt. 1, AIAA, Washington, DC, 1994, pp. 170-194.
6. Newsome, R. W., Walters, R. W., and Thomas, J. L., "An Efficient Strategy for Upwind Relaxation Solutions to the Thin-Layer Navier-Stokes Equations," AIAA Journal, Vol. 27, No. 9, 1989, pp. 1165-1166; also AIAA Paper 87-1113, June 1987.
7. Burgreen, G. W., and Baysal, O., "Three-Dimensional Aerodynamic Shape Optimization of Wings Using Sensitivity Analysis," AIAA Paper 94-0094, Jan. 1994.
8. Burgreen, W. G., "Three-Dimensional Aerodynamic Shape Optimization of Wings Using Discrete Sensitivity Analysis," Ph.D. Dissertation, Old Dominion Univ., Norfolk, VA, May 1994.
9. Jameson, A., "Optimum Aerodynamic Design Via Boundary Control," Optimum Design Methods in Aerodynamics, AGARD, FDPVKI, Von Kármán Inst., Rhode-St. Genese, Belgium, April 1994.
10. Taylor, A. C., III, Newman, P. A., Hou, G. J.-W., and Jones, H. E., "Recent Advances in Steady Compressible Aerodynamic Sensitivity Analysis," Flow Control, Mathematics and Its Applications, edited by M. D. Gunsberger, Vol. 68, Springer-Verlag, New York, 1995, pp. 341-356.
11. Sherman, L. L., Taylor, A. C., III, Green, L. L., Newman, P. A., Hou, G. J.-W., and Korivi, V. M., "First- and Second-Order Aerodynamic Sensitivity Derivatives Via Automatic Differentiation with Incremental Iterative Methods," Journal of Computational Physics, Vol. 129, 1996, pp. 307-336; also AIAA Paper 94-4262, Sept. 1994.
12. Barger, R. L., and Adams, M. S., "Automatic Computation of Wing-Fuselage Intersection Lines and Fillet Inserts with Fixed-Area Constraint," NASA TM 4406, March 1993.
13. Barger, R. L., Adams, M. S., and Krishnan, R. R., "Automatic Computation of Euler Marching Grids and Subsonic Grids for Wing-Fuselage Configurations," NASA TM 4573, July 1994.
14. Unger, E. R., and Hall, L. E., "The Use of Automatic Differentiation in an Aircraft Design Problem," AIAA/USAF/NASA/ISSMO 5th Symposium on Multidisciplinary Analysis and Optimization, Pt. 1, AIAA, Washington, DC, 1994, pp. 64-72.
15. Rall, L. B., "Automatic Differentiation: Techniques and Applications," Recent Development and Applications, Lecture Notes in Computer Science and Mathematical Programming, Vol. 120, Springer-Verlag, Berlin, 1981.
16. Griewank, A., and Corliss, G. F. (eds.), Automatic Differentiation of Algorithms: Theory., Implementation, and Application, Society of Industrial and Applied Mathematics, Philadelphia, PA, 1991.
17. Bischof, C. H., Carle, A., Corliss, G. F., Griewank, A., and Hovland, P., "ADIFOR: Generating, Derivative Codes from Fortran Programs," Scientific Programming, Vol. 1, No. 1, 1992, pp. 1-29.
18. Bischof, C. H., and Griewank, A., "ADIFOR: A Fortran System for Portable Automatic Differentiation," AIAA/USAF/NASA/OAI 4th Symposium on Multidisciplinary Analysis and Optimization, Pt. 1, AIAA, Washington, DC, 1992, pp. 433-441.
19. Bischof, C. H, Carle, A., Corliss, G. F., Griewank, A., and Hovland, P., "Getting Started with ADIFOR. ADIFOR Working Note #9," Mathematics and Computer Science Division, Argonne National Lab., MCS-ANL-TM-164, Argonne, IL, 1992.
20. Vanderplaats, G. N., "ADS - A Fortran Program for Automated Design Synthesis," NASA CR-17785, Sept. 1985.
21. Barthelemy, J.-F. M., Wrenn, G. A., Dovi, A. R., Coen, P. G., and Hall, L. E., "Supersonic Transport Wing Minimum Weight Design Integrating Aerodynamics and Structures," Journal of Aircraft, Vol. 31, No. 2, 1994, pp. 330-338.