3-D hypersonic inlet optimization using a genetic algorithm

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Chernyavsky, B ^a   Stepanov, V ^a   Rasheed, K ^b   Blaize, M ^b   Knight, D ^b  

^a CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

^b RUTGERS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; CODES (SYMBOLS); FLOW SEPARATION; GENETIC ALGORITHMS; HYPERSONIC INLETS; INTAKE SYSTEMS; MACH NUMBER; PROPULSION; RECOVERY; TURBULENCE;

AERODYNAMIC OPTIMIZATION; INLET CONFIGURATION; INLET PERFORMANCE; OPTIMIZATION CRITERIA; OPTIMIZING PARAMETERS; TOTAL PRESSURE RECOVERY; TOTAL PRESSURE RECOVERY COEFFICIENT; TURBULENT BOUNDARY LAYERS;

OPTIMIZATION;

EID: 33845398814     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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2. V. Shukla, A. Gelsey, M. Schwabacher, D. Smith and D. Knight. “Automated Design Optimization for the P2 and P8 Hypersonic Inlets”, Journal of Aircraft, Vol. 34, No. 2, March-April 1997, pp 228-235.
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4. M. Blaize, D. Knight and K. Rasheed, “Automated Optimal Design of Two Dimensional High Speed Missile Inlets”, AIAA Paper 98-0950.
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10. V. Vinogradov, V. Stepanov and M. Goldfeld, “Experimental and Numerical Investigations of Two Concepts of Hypersonic Inlet”, AIAA-95-2721.
11. K. Rasheed, H. Hirsh and A. Gelsey, “A Genetic Algoritm for Continuous Design Space Search”, Artifical Intelligence in Engineering, Vol.11, No.3, p.295.
12. D.E. Goldberg, “Genetic Algorithm in Search, Optimization, and Machine Learning”, Addison-Wesley, Reading, Mass., 1989.