HSCT configuration design using response surface approximations of supersonic euler aerodynamics

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Knill, Duane L ^a   Giunta, Anthony A ^a   Baker, Chuck A ^a   Grossman, Bernard ^a   Mason, William H ^a   Haftka, Raphael T ^a   Watson, Layne T ^a  

^a State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; COMPUTATIONAL FLUID DYNAMICS; CONSTRAINED OPTIMIZATION; DESIGN AIDS; NUMERICAL METHODS; REGRESSION ANALYSIS; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; SURFACE PROPERTIES;

AERODYNAMIC PREDICTIONS; COARSE-GRAINED PARALLELS; COMPUTATIONAL FLUID DYNAMICS ANALYSIS; HIGH SPEED CIVIL TRANSPORTS; MULTIDISCIPLINARY DESIGN OPTIMIZATION; RESPONSE SURFACE APPROXIMATION; STEPWISE REGRESSION ANALYSIS; VARIABLE COMPLEXITY MODEL;

AERODYNAMIC CONFIGURATIONS;

EID: 85085847521     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-905     Document Type: Conference Paper

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