Parallel unsteady overset mesh methodology for a multi-solver paradigm with adaptive cartesian grids

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2008, Pages

  Sitaraman, Jayanarayanan ^a,c,g   Floros, Matt ^a,d,g   Wissink, Andrew M ^b,e,g   Potsdam, Mark ^b,f,g  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c NIA   (United States)

^d U S ARMY RESEARCH LABORATORY   (United States)

^e Scaled Numerical Physics LLC

^f US Army AMRDEC Development   (United States)

^g AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DATA TRANSFER; FLIGHT SIMULATORS; MESH GENERATION;

ADAPTIVE CARTESIAN GRID; ADAPTIVE MESH REFINEMENT; COMPUTATIONAL DOMAINS; COMPUTATIONAL INFRASTRUCTURE; DATA INTERPOLATION; IMPLICIT HOLE CUTTINGS; NEAR-WALL EFFECTS; USER INTERVENTION;

COMPUTATIONAL FLUID DYNAMICS;

EID: 85067322064     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-7177     Document Type: Conference Paper

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