Multicriteria design optimization of a supersonic inlet based upon global missile performance

Journal of Propulsion and Power

Volumn 20, Issue 3, 2004, Pages 542-558

  Gaiddon, A ^a,d   Knight, D D ^b,e   Poloni, C ^c,f  

^a Matra Bae Dynam Aerospat A France   (France)

^b RUTGERS UNIVERSITY   (United States)

^c UNIVERSITY OF TRIESTE   (Italy)

^d Vehicle Department   (France)

^e Department of Mechanical Engineering ^*

^f 24

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; GENETIC ALGORITHMS; MISSILES; NAVIER STOKES EQUATIONS; NOZZLES; OPTIMIZATION; PROPULSION;

COMBUSTION EFFICIENCY; MACH NUMBER; STOICHIOMETRIC COEFFICIENT; THRUST COEFFICIENT;

SUPERSONIC AERODYNAMICS;

EID: 2942538006     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.2390     Document Type: Article

References (33)

1. Sedon, J., and Goldsmith, E., Practical Intake Aerodynamic Design, AIAA, Washington, D.C., 1993.
2. Mahoney, J., Inlets for Supersonic Missiles, AIAA, Washington, D.C., 1999.
3. Deb, K., Multi-Objective Optimization Using Evolutionary Algorithms, Wiley, New York, 2001.
4. Gaiddon, A., and Pagan, D., "Design Methodology for Supersonic Air Intakes," AIAA Paper 2001-3881, July 2001.
5. Bourdeau, C., Blaize, M., and Knight, D., "Performance Analysis for High-Speed Missile Inlets," Journal of Propulsion and Power, Vol. 16, No. 6, 2000. pp. 1125-1131.
6. Montazel, X., Kergaravat, Y., and Blaize, M., "Navier-Stokes Simulation Methodology for Supersonic Missile Inlets," Proceedings of the International Symposiumon Airbreathing Engines, Paper 97-7029, Sept. 1997.
7. Berkowitz, B., "Information Age Intelligence," Foreign Policy, Vol. 103, June 1996, pp. 35-50.
8. Shukla, V., Gelsey, A., Schwabacher, M., Smith, D., and Knight, D., "Automated Design Optimization for the P2 and P8 Hypersonic Inlets," Journal of Aircraft, Vol. 34, No. 2, 1997, pp. 228-235.
9. Zha, G.-C, Smith, D., Schwabacher, M., Rasheed, K., Gelsey, A., and Knight, D., "High-Performance Supersonic Missile Inlet Design Using Automated Optimization," Journal of Aircraft, Vol. 34, No. 6, 1997, pp. 697-705.
10. Blaize, M., Knight, D., and Rasheed, K., "Automated Optimal Design of Two-Dimensional Supersonic Missile Inlets," Journal of Propulsion and Power, Vol. 14, No. 6, 1998, pp. 890-898.
11. Kergaravat, Y., Vives, E., and Knight, D., "Inlet/Body Integration Preliminary Design for Supersonic Air-Breathing Missiles Using Automated Multi-Disciplinary Optimization," Proceedings of the RTO AVT Symposium on Aerodynamic Design and Optimization of Flight Vehicles in a Concurrent Multi-Disciplinary Environment, RTO-AVT, Ottawa, Oct. 1999.
12. Gaiddon, A., and Knight, D., "Multi-Criteria Design Optimization of Integrated Three-Dimensional Supersonic Inlets," Journal of Propulsion and Power, Vol. 19, No. 3, 2003.
13. Knight, D., "Application of Genetic Algorithms to High Speed Air Intake Design," Lecture Series Programme 1999-2000, Von Karman Inst. for Fluid Dynamics, Rhode-Saint-Genese, VKILS 2000-07, Belgium, May 2000.
14. Knight, D., "Automated Optimal Design of Supersonic and Subsonic Diffusers Using CFD," ECCOMAS 2000, Barcelona, Spain, Sept. 2000.
15. GASPex v4.1 Reference Guide, AeroSoft, Inc., Blacksburg, VA, 2001.
16. Hexa User's Manual, ICEMCFD Engineering GmbH, München, Germany, 1999.
17. Love, E., "Base Pressure at Supersonic Speeds on Two-Dimensional Airfoils and on Bodies of Revolution," NACA TN 3819, Jan. 1957.
18. Carrière, P., "Aérodynamique Interne des Réacteurs," ENSAE Supaero, Toulouse, France, July 1977.
19. Pagan, D., and Lacau, R., "Missile Aerothermodynamics and Propulsion Integration," AGARD, AGARD-R-813, Orléans, France, Oct. 1996.
20. Nelder, J., and Mead, R., "A Simplex Method for Function Minimization," The Compututer Journal, Vol. 7, No. 7, 1965, pp. 308-313.
21. Collins, R., and Jefferson, D., "Selection in Massively Parallel Genetic Algorithms," Fourth International Conference on Genetic Algorithms, edited by Morgan-Kaufman, San Matco, CA, 1991.
22. Yamamoto, K., and Inoue, O., "New Evolutionary Direction Operator for Genetic Algorithms," AIAA Journal, Vol. 33, No. 10, 1995, pp. 1990-1993.
23. Horn, J., and Nafpliotis, N., "Multiobjective Optimization Using the Niched Pareto Genetic Algorithm," IlliGAL, Rept. 93005, Univ. of Illinois at Urbana-Champaign, Urbana, April 1993.
24. Belegundu, A. D., Murthy, D. V., Salagame, R. R., and Constants, E. W., "Multiobjective Optimization of Laminated Ceramic Composites Using Genetic Algorithms," Fifth AIAA/USAF/NASA Symposium on Multi-disciplinary Analysis and Optimization, AIAA Paper 84-4363-CP, Panama City, Florida, 1994, pp. 1015-1022.
25. Michielssen, E., and Weile, D., "Electromagnetic System Design Using Genetic Algorithms," Genetic Algorithms in Engineering and Computer Science, Wiley, New York, 1995, pp. 345-369.
26. Goldberg, D., Genetic Algorithms in Search, Optimization and Machine Learning, Addison Wesley, Longman, Reading, VLA, 1998.
27. Hajela, P., "Genetic Search Strategies in Multicriterion Optimal Design," Structural Optimization, Vol. 4, Springer-Verlag, 'Berlin, 1992, pp. 99-107.
28. Schwefel, H., Evolution and Optimum Seeking, Wiley, New York, 1995.
29. Rechenberg, I., Evolutionstrategie: Optimierung Technisher Systeme nach Prinzipien des Biologischen Evolution, Fromman-Hozlboog Verlag, Stuttgart, 1973.
30. Bourdeau, C., Blaize, M., and Knight, D., "Performance Analysis for an Automated Optimal Design of High Speed Inlets," AIAA Paper 99-0611, Jan. 1999.
31. Johnston, J., "Diffuser Design and Performance Analysis by Unified Integral Methods," AIAA Paper 97-2733, July 1997.
32. Sobol, I., Die Monte-Carlo Methode, Deutscher Verlag der Wissenschaften, Berlin, Germany, 1991.
33. Gaiddon, A., Gréard, J., and Pagan, D., "Automated Optimization of Supersonic Missile Performance Taking into Account Design Uncertainties," AIAA Paper 2003-3879, June 2003.