Computational study of Reynolds number and angle-of-attack effects on a 1303 ucav configuration with a high-order overset-grid algorithm

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Sherer, Scott E ^a   Visbal, Miguel R ^a   Gordnier, Raymond E ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CHORD; ANGLES OF ATTACK; COMPUTATIONAL APPROACH; COMPUTATIONAL STUDIES; DOMAIN DECOMPOSITIONS; GRID GENERATION; GRID TECHNIQUES; HIGH-ORDER; PARALLEL PROCESSING; SPATIAL SCHEME; TURBULENCE MODELING; UNRESOLVED SCALE;

AEROSPACE ENGINEERING; ANGLE OF ATTACK; DOMAIN DECOMPOSITION METHODS; HYDRAULICS; MATHEMATICAL OPERATORS; REYNOLDS NUMBER;

MESH GENERATION;

EID: 78549246833     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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