Multi-point nose shape optimization of space launcher using response surface method

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Lee, Jae Woo ^a   Min, Byung Young ^a   Byun, Yung Hwan ^a   Kim, Sang Jin ^b,c  

^a Konkuk University   (South Korea)

^b Agency for Defence Development   (South Korea)

^c 3rd Research and Development Center ^*  (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894350028     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. J.-W. Lee and J. Y. Hwang, " The Conceptual Design of Air-Launching Micro Space Launcher, Mirinae-1, " Journal of Korean Society for Aeronautical and Space Sciences, Vol. 29, No. 2, March, 2001.
2. J. O. Hager, S. Eyi, and K. D. Lee, "Two-Point Transonic Airfoil Design Using Optimization for Improved Off-Design Performance, " Journal of Aircraft, Vol. 31, No. 5, Sept.-Oct, 1994.
3. H.-J. Kirn and O.-H. Rho, "Dual-Point Design of Transonic Airfoils Using the Hybrid Inverse Optimization Method, " Journal of Aircraft, Vol. 34. No. 5, Sept-Oct. 1997.
4. Anthony A. Giunta, Vladimir Balabanov, Dan Haim, Bernard Grossman, William H. Mason, Layne T. Watson, and Raphael T. Haftka, "Wing Design for a High-Speed Civil Transport Using a Design of Experiments Methodology, " AIAA-96-4001-CP, September 1996.
5. S.-J. Kirn, K.-S. Jeon, and J.-W. Lee, "Optimal Design of a Space Launch Vehicle Using Response Surface Method, " AIAA 2000-4866, Sept. 2000.
6. Myers, R. H. and Montgomery, D. C., Response Surface Methodology, John Wiley & Sons Inc., 1995.
7. Burgee, S., Giunta, A. A., Balabanov, V., Grossman, B., Mason, W. H., Narducci, R., Haftka, R. T., and Watson, L., "A Coarse-Grained Parallel Variable-Complexity Multidisciplinary Optimization Paradigm, " The International Journal of Supercomputing Applications and High Performance Computing, Vol. 10, No. 4, 1996, pp 269-299.
8. J.-S. Tak, A Study on the Numerical Simulation of the Shock Tunnel, Master's Thesis, Konkuk University, 2000.
9. Ames Research Staff, "Equations, Tables, and Charts for Compressible Flow, " NACA R-1135, 1953.
10. Holden, M. S. and Moselle, J. R., " Theoretical and Experimental Studies of the Shock Wave-Boundary Interaction on Compression Surfaces in Hypersonic Flow, " AIAA 89-0458, Jan. 1989.
11. Rudy, D. H., Thomas, J. L., Kumar, A., Gnoffo, P., and Chakravarthy, S. R., " A Validation Study of Four Navier-Stokes Codes for High-Speed Flows, " AIAA 89-1838, June 1989.
12. J. Y. Lee and M. J. Lewis, "Numerical Study of the Flow Establishment Time in Hypersonic Shock Tunnels, " Journal of Spacecraft and Rockets, Vol. 30, No. 2, Mar. 1993, pp. 152-163.
13. Jeong-Soo Tak, Yung-Hwan Byun, Jae-Woo Lee, Jang-Yeon Lee, Chul-Jun Huh, and Byung-Chul Choi, "A Numerical Study on the Performance Analysis of Shock Tunnel, " Proceedings of the Korea Society of Computational Fluids Engineering Spring Annual Meeting, May 2000.
14. Vanderplaats G. N. and Hicks R. M., "Numerical Airfoil Optimization Using a Reduced Number of Design Coordinates, " NASA TM X-73151, 1976.
15. Jae-Woo Lee, Young-Ki Lee, and Yung-Hwan Byun, "The Design of Space Launch Vehicle Using Numerical Optimization and Inverse Method, " Journal of Spacecraft and Rockets, Vol. 38, No. 2, Mar. 2001.
16. Leslie Piegl and Wayne Tiller, "Curve and Surface Constructions Using Rational B-Splines, " Computer Aided Design, Vol. 19, No. 9, 1987, pp. 485-498.
17. Wayne Tiller, "Rational B-Splines for Curve and Surface Representation, " IEEE Computer Graphics and Application, Vol. 3, No. 6, 1983, pp. 61-69.
18. H. Olivier, "Influence of the Velocity Gradient on the Stagnation Point Heating in Hypersonic flow", Shock Waves, Vol. 5, 1995, pp. 205-216.
19. John J. Bertin, Hypersonic Aerothermodynamics, AIAA Education Series, 1994, pp. 240-259.
20. DOT Users Manual, Vanderplaats Research & Development, Inc., 1995.
21. Michalewicz, Z., Genetic Algorithms + Data Structures-Evolution Programs, Springer-Verlag, 1996.
22. K.-S. Jeon, S.-J. Kirn, and J.-W. Lee, "Application of Response Surface Method for the Highly Nonlinear Optimization Problems, " Proceedings of the KSAS Spring Annual Meeting, Apr. 2000.
23. Anthony A. Giunta, Aircraft Multidisciplinary Design Optimization Using Design of Experiments Theory and Response Surface Modeling Methods, Ph.D. Thesis, Virginia Polytechnic Institute and State University, 1997.
24. Y.-S. Chae et al, "Research and Development of KSR-III(I) Final Report, " Korea Aerospace Research Institute, 1998.