High-performance supersonic missile inlet design using automated optimization

Journal of Aircraft

Volumn 34, Issue 6, 1997, Pages 697-705

  Zha, Ge Cheng ^a,d   Smith, Donald ^b,d   Schwabacher, Mark ^b   Rasheed, Khaled ^b   Gelsey, Andrew ^b,d   Knight, Doyle ^a,d   Haas, Martin ^c,d  

^a RUTGERS UNIVERSITY   (United States)

^b RUTGERS UNIVERSITY   (United States)

^c UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; GENETIC ALGORITHMS; MISSILES; NAVIER STOKES EQUATIONS; OPTIMIZATION; SUPERSONIC FLOW;

MACH NUMBER; MULTISTART GRADIENT LINE SEARCH OPTIMIZERS;

INTAKE SYSTEMS;

EID: 0031268442     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2241     Document Type: Article

References (15)

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