Multidisciplinary design optimization of supersonic fighter wing using response surface methodology

9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 2002, Pages

  Kim, Yushin ^a   Lee, Dong Ho ^a   Kim, Yonghyup ^a   Yee, Kwanjung ^b  

^a Seoul National University   (South Korea)

^b Korea Aerospace Research Institute (KARI)   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROELASTICITY; AIRFOILS; ASPECT RATIO; DESIGN AIDS; STRUCTURAL DESIGN; SURFACE PROPERTIES;

AERO-DYNAMIC PERFORMANCE; AEROELASTIC ANALYSIS; BETTER PERFORMANCE; HIGH ANGLE OF ATTACK; MULTIDISCIPLINARY DESIGN OPTIMIZATION; RESPONSE SURFACE METHODOLOGY; SPANWISE LOCATIONS; STRUCTURAL PERFORMANCE;

SHAPE OPTIMIZATION;

EID: 31144431901     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (26)

1. Zang, T. A., and Green, L. L., "Multidisciplinary Design Optimization Techniques: Implications and Opportunities for Fluid Dynamics," AIAA Paper, AIAA 99-3798.
2. Sobieszczanski-Sobieski, J., and Haftka, R. T., "Multidisciplinary Aerospace Design Optimization: Survey of Recent Developments," AIAA Paper, AIAA 96-3798.
3. Lollo, A., and Salas, M. D., "Optimum Transonic Airfoils Based on the Euler Equations," NASA CR- 201638.
4. Ahn, J. K., Kim, H. J., Lee, D. H., and Rho, O. H., "Response Surface Method for Aircraft Design in Transonic Flow," Journal of Aircraft, Vol. 38, No. 2, 2001, pp. 231-238.
5. Venkataraman, P., "Low Speed Multi-Point Airfoil Design," AIAA Paper, AIAA 98-2402.
6. Arian, E., and Vatsa V. N., "A Preconditioning Method for Shape Optimization Governed by the Euler Equations," NASA CR-1998-206926.
7. Somearwoto, B., "The Variational Method for Aerodynamic Optimization Using the Navier-Stokes Equations," NASA CR-97-206277.
8. Campbell, R. L., "Efficient Viscous Design of Realistic Aircraft Configurations," AIAA Paper, AIAA 98-2539.
9. Chen, H. H., Chang, K. C., Tzong, T., and Cebeci, T., "Aeroelastic Analysis of Wing and Wing/Fuselage Configurations," AIAA Paper, AIAA 98-0907.
10. Gern, F. H., and Librescu, L., "Static and Dynamic Aeroelasticity of Advanced Aircraft Wings Carrying External Stores," AIAA Journal, Vol. 36, No. 7, 1998, pp. 1121-1129.
11. Newsome, R. W., Berkooz, G., and Bhaskaran, R., "Use of Analytical Flow Sensitivities in Static Aeroelasticity," AIAA Journal, Vol. 36, No. 8, 1998, pp.1537-1540.
12. Farhat, C., Lesoinne, M., and Let-aleTal/et-allec, P., "Load and Motion Transfer Algorithms for Fluid/Structure Interaction Problems with Non-Matching Discrete Interfaces: Momentum and Energy Conservation, Optimal Discretization and Application to Aeroelasticity," Computer Methods in Applied Mechanics and Engineering, Vol. 157, 1998, pp. 95-114.
13. Li, G., and Grandhi, R., "Accuracy and Efficiency Improvement of Response Surface Methodology for Multidisciplinary Design Optimization," AIAA Paper, AIAA 2000-4715.
14. Samareh, J. A., and Bhatia, K. G., "A Unified approach to Modeling Multidisciplinary Interactions," AIAA Paper, AIAA 2000-4704.
15. Samareh, J. A., "Multidisciplinary Aerodynamic- Structural Shape Optimization Using Deformation(MASSOUD)," AIAA Paper, AIAA 2000-4911.
16. Nydick, I., and Friedmann, P. P., "Aeroelastic Analysis of a Trimmed Generic Hypersonic Vehicle," AIAA Paper, AIAA 98-1807.
17. Guinta, A. A., "Aircraft Multidisciplinary Design Optimization Using Design of Experiment Theory and Response Surface Modeling Methods," Ph. D. Dissertation, Department of Aerospace Engineering, Virginia Polytechnic Institute and State University, May 1997, Blacksburg, VA.
18. Sevant, N. E., Bloor, M. I. G., and Wilson, M. J., "Cost-Effective Multipoint Design of a Blended HSCT," AIAA Paper, AIAA 98-2785.
19. Reuther, J., Alonso, J. J., Rimlinger, M. J., and Jameson, A., "Aerodynamic shape Optimization of Supersonic Aircraft Configurations via an Adjoint Formulation on Distributed Memory Parallel Computers," Computers and Fluids, Vol. 28, 1999, pp.675-700.
20. Burgee, S., Guinta, A. A., Balalbanov, V., Grossman, B., Mason, W. H., Narducci, R., Haftka, R. T., and Watson, L. T., "A Coarse-Grained Parallel Variable-Complexity Multidisciplinary Optimization Paradigm," The International Journal of Supercomputer Applications and High Performance Computing, Vol. 10, No. 4, 1996, pp.269-299.
21. Kim, Y., Kim, J., Jeon, Y., Bang, J., Lee, D. H., Kim, Y., and Park, C., "Multidisciplinary Aerodynamic-Structural Design Optimization of Supersonic Fighter Wing Using Response Surface Methodology," AIAA Paper, AIAA 2002-0322
22. Myers, R. H., and Montgomery, D. C., Response Surface Methodology: Process and Product Optimization Using Designed Experiments, John Wiley & Sons, New York, 1995.
23. Rhiu, J. J., "A New Efficient Formulation for Finite Element Analysis of Thin Shell Structures Undergoing small and Large Deflection," Ph. D. Dissertation, Department of Aerospace Engineering, University of Maryland, 1985.
24. Cook, R. D., Malkus, D. S., and Plesha, M. E., Concepts and applications of Finite Element Analysis, 3rd edition, John Wiley & Sons, New York.
25. Chapra, S. C., Canale, R. P., Numerical Methods for Engineers, McGraw-Hill, International editions.
26. Eschenauer, H., Koski, J., and Osyczka, A., Multicriteria Design Optimization, Springer-Verlag, 1990.