Multifidelity response surface model for hsct wing bending material weight

7th AIAA/USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization

Volumn , Issue , 1998, Pages 778-788

  Balabanov, Vladimir ^a   Haftka, Raphael T ^b   Grossman, Bernard ^c,d   Mason, William H ^c,d   Watson, Layne T ^c  

^a Vanderplaats Research and Development Inc   (United States)

^b J Crayton Pruitt Family Department of Biomedical Engineering   (United States)

^c VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^d Virginia Polytechnic Institute and State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DUCTS; SHAPE OPTIMIZATION; STRUCTURAL OPTIMIZATION; SURFACE PROPERTIES;

AERODYNAMIC OPTIMIZATION; COARSE FINITE ELEMENT MODEL; HIGH FIDELITY ANALYSIS; HIGH SPEED CIVIL TRANSPORTS; LOW FIDELITY ANALYSIS; RESPONSE SURFACE MODELING; RESPONSE SURFACE MODELS; RESPONSE SURFACE TECHNIQUES;

FINITE ELEMENT METHOD;

EID: 84983206766     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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