Unsteady flow calculations with a parallel multiblock moving mesh algorithm

AIAA Journal

Volumn 39, Issue 6, 2001, Pages 1021-1029

  Tsai, H M ^a,c,d   Wong, A S F ^a   Cai, J ^b,e   Zhu, Y ^b   Liu, F ^b  

^a DSO NATIONAL LABORATORIES   (Singapore)

^b University of California at Irvine   (United States)

^c Aeronautical Systems Program   (United States)

^d NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

^e NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ALGORITHMS; BOUNDARY CONDITIONS; CALCULATIONS; COMPUTER SIMULATION; FLUTTER (AERODYNAMICS); INTERPOLATION; ITERATIVE METHODS; NAVIER STOKES EQUATIONS; UNSTEADY FLOW; WINGS;

ARC LENGTH BASED TRANSFINITE INTERPOLATION; BODY FITTED GRIDS; GRID DEFORMATION METHOD; MULTIBLOCK PARALLEL UNSTEADY FLOW CALCULATIONS; MULTIGRID AND DUAL TIME STEPPING; PARALLEL DYNAMIC MOVING MESH ALGORITHM; SMOOTHING OPERATOR; SPRING NETWORK APPROACH;

AERODYNAMICS;

EID: 0035369438     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1442     Document Type: Article

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