Geometry parameterization method for multidisciplinary applications

AIAA Journal

Volumn 47, Issue 6, 2009, Pages 1568-1578

  Anderson, W Kyle ^a,b   Karman, Steve L ^a,b   Burdyshaw, Chad ^a,b  

^a UNIVERSITY OF TENNESSEE AT CHATTANOOGA   (United States)

^b SimCenter: National Center for Computational Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL GRIDS; CURRENT TECHNIQUES; DESIGN OPTIMIZATION; FREE-FORM DEFORMATION; GEOMETRY PARAMETERIZATION; MULTIDISCIPLINARY DESIGN OPTIMIZATION; NUMERICAL SIMULATION; PARAMETERIZING; THREE DIMENSIONS;

COMBINATORIAL OPTIMIZATION; MULTI AGENT SYSTEMS;

DEFORMATION;

EID: 67650930701     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.41101     Document Type: Conference Paper

References (35)

1. Hicks, R. M., and Henne, P. A., "Wing Design by Numerical Optimization," Journal of Aircraft, Vol.15, No.7, 1978, pp. 407-412. doi:10.2514/3.58379 (Pubitemid 8614433)
2. Angrand, F., "Optimum Design for Potential Flows," International Journal for Numerical Methods in Fluids, Vol.3, 1983, pp. 265-282. doi:10.1002/fld.l650030306 (Pubitemid 13540025)
3. Jameson, A., "Aerodynamic Design via Control Theory," Journal of Scientific Computing, Vol.3, 1988, pp. 233-260. doi:10.1007/BF01061285
4. Drela, M., "Design and Optimization Method for Multi-Element Airfoils," AIAA Paper 93-0969, Feb. 1993.
5. Burgreen, G. W., and Baysal, 0., "Three-Dimensional Aerodynamic Shape Optimization of Wings Using Sensitivity Analysis," AIAA Paper 94-10094, Jan. 1994.
6. Jameson, A., Alonso, J. J., Reuther, J., Martinelli, L., and Vassberg, J. C, "Aerodynamic Shape Optimization Techniques Based on Control Theory," AIAA Paper 98-2538, 1998.
7. Anderson, W. K., and Venkatakrishnan, V., "Aerodynamic Design Optimization on Unstructured Grids with a Continuous Adjoint Formulation," Computers and Fluids, Vol.28, Nos. 4-5, 1999, pp. 443-480. doi:10.1016/S0045- 7930(98)00041-3 (Pubitemid 29346194)
8. Anderson, W. K., and Bonhaus, D. L., "Airfoil Design on Unstructured Grids for Turbulent Flows," AIAA Journal, Vol.37, No.2, 1999, pp. 185-191. doi: 10.2514/2.712
9. Nielsen, E. J., and Anderson, W. K., "Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations," AIAA Journal, Vol.37, No.11, 1999, pp. 1411-1419. doi: 10.2514/2.640 (Pubitemid 30512800)
10. Burdyshaw, C. E., "Quasi 3D Multi-Stage Turbomachinery Pre- Optimizer," M.S. Thesis, Mississippi State Univ., Mississippi State, MS, 2001.
11. Nielsen, E. J., and Anderson, W. K., "Recent Improvements in Aerodynamic Optimization on Unstructured Meshes," AIAA Journal, Vol.40, No.6, 2002, pp. 1155-1163. doi:10.2514/2.1765 (Pubitemid 34648448)
12. Kim, H., Koc, S., andNakahashi, K., "Surface Modification Method for Aerodynamic Design Optimization," AIAA Journal, Vol.43, No.4, April 2005, pp. 727-740. doi: 10.2514/1.11181
13. Fudge, D. M., and Zingg, D. W., "A CAD-Free and a CAD-Based Geometry Control System for Aerodynamic Shape Optimization," AIAA Paper 2005-0451, 2005.
14. Samareh, J. A., "A Novel Shape Parameterization Approach," NASA TM/TM-1999-209116, May 1999.
15. Samareh, J. A., "A Survey of Shape Parameterization Techniques for High-Fidelity Multidisciplinary Shape Optimization," AIAA Journal, Vol.39, May 2001, pp. 877-884. doi:10.2514/2.1391 (Pubitemid 32471217)
16. Smith, R. E., Bloor, M. L. G., Wilson, M. J., and Thomas, A. M., "Rapid Airplane Parametric Input Design," AIAA Paper 95-1687, 1995.
17. Leiva, J. P., and Watson, B. C, "Automatic Generation of Basis Vectors for Shape Optimization in the GENESIS program," AIAA Paper 1998- 4852, Sept. 1998.
18. Samareh, J. A., "Multidisciplinary Aerodynamic-Structural Shape Optimization Using Deformation (MASSOUD)," AIAA Paper 2000- 4911,2000.
19. Samareh, J. A., "Aerodynamic Shape Optimization Based on FreeForm Deformation," AIAA Paper 2004-4630, 2004.
20. Sarakinos, S. S., Amoiralis, E., and Nikolos, I. K., " ExploringFreeform Deformation Capabilities in Aerodynamic Shape Parameterization," International Conference on Computer as a Tool, 2005, pp. 535-538.doi:10.1109/EURCON.2005.1629983 (Pubitemid 46389084)
21. Venkatakrishnan, V., and Mavriplis, D. J., "Implicit Method for the Computation of Unsteady Flows on Unstructured Grids," Journal of Computational Physics, Vol.127, 1996, pp. 380-397. doi:10.1006/jcph.l996.0182 (Pubitemid 126171079)
22. Yang, Z., and Mavriplis, D. J., "Mesh Deformation Strategy Optimized by the Adjoint Method on Unstructured Meshes," AIAA Journal, Vol.45, No.12, 2007, pp. 2885-2896. doi:10.2514/l .30592
23. Truong, A., Oldfield, C. A., and Zingg, D. W., "Mesh Movement for a Discrete-Adjoint Newton-Krylov Algorithm for Aerodynamic Optimization," AIAA Journal, Vol.46, No.7, July 2008, pp. 1695- 1704. doi:10.2514/l .33836
24. Fox, P. A., Hall, A. D., and Schryer, N. L., "The PORT Mathematical Subroutine Library," Transactions on Mathematical Software, Vol.4, No.2, June 1978, pp. 104-126.doi:10.1145/355780.355783
25. Pirzadeh, S., "Structured Background Grids for Generation of Unstructured Grids by Advancing-Front Method," AIAA Journal, Vol.31, No. 2, 1993, pp. 257-265. doi: 10.2514/3.11662
26. Anderson, W. K., and Bonhaus, D. L., "An Implicit Upwind Algorithm for Computing Turbulent Flows on Unstructured Grids," Computers and Fluids, Vol.23, No.1, 1994, pp. 1-21. doi:10.1016/0045-7930(94)90023-X
27. Anderson, W. K., Newman, J. C, Whitfield, D. L., and Nielsen, E. J., "Sensitivity Analysis for the Navier-Stokes Equations on Unstructured Meshes Using Complex Variables," AIAA Journal, Vol.39, No.1, 2001, pp. 56-63. doi:10.2514/2.1270 (Pubitemid 32872423)
28. Newman, J. C, Anderson, W. K., and Whitfield, D. L., " Multidisciplinary Sensitivity Derivatives Using Complex Variables," Mississippi State Univ. MSSU-COE-ERC-98-108, 1998.
29. Newman, J. C, Anderson, W. K., and Whitfield, D. L., "A Step-Size Independent Approach to Multidisciplinary Sensitivity Analysis," Journal of Aircraft, Vol.40, No.3, 2003, pp. 566-573. doi:10.2514/2.3131
30. Cook, P. H., McDonald, M. A., and Firmin, M. C. P., "Aerofoil RAE 2822-Pressure Distributions, and Boundary Layer and Wake Measurements," Experimental Data Base for Computer Program Assessment, AGARD Rept. AR 138, 1979.
31. Whitcomb, R. T., and Clark, L. R., "An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers," NASA TM X-1109, 1965.
32. Sreenivas, K., Hyams, D. G., Nichols, D. S., Mitchell, B., Taylor, L. K., Briley, W. R., and Whitfield, D. L., "Development of an Unstructured Parallel Flow Solver for Arbitrary Mach Numbers," AIAA Paper 2005-10325, Jan. 2005.
33. Sreenivas, K., Taylor, L., and Briley, R., "A Global Preconditioner for Viscous Flow Simulations at AU Mach Numbers," AIAA Paper 2006-3852, June 2006.
34. Burdyshaw, C. E., and Anderson, W. K., "A General and Extensible Unstructured Mesh Adjoint Method," Journal of Aerospace Computing, Information, and Communication, Vol.2, No.10, 2005, pp. 401-413. doi:10.2514/l. 15932 (Pubitemid 41426894)
35. Burdyshaw, C. E., "Achieving Automatic Concurrency Between Computational Field Solvers and Adjoint Sensitivity Codes," Ph.D. Thesis, Univ. of Tennessee, Chattanooga, TN, May 2006.