Complex configuration meshing - An industrial view and approach

16th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2003, Pages

  Hitzel, Stephan M ^a   Tremel, Udo ^a   Deister, Frank ^a   Rieger, Herbert ^a  

^a AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPLEX CONFIGURATION; COMPUTATIONAL DEMANDS; DISTRIBUTED MEMORY ARCHITECTURE; EFFICIENT SIMULATION; MULTI-BODY CONFIGURATIONS; NAVIER STOKES SIMULATION; OPTIMIZED PERFORMANCE; TIME DEPENDENT SIMULATION;

AERODYNAMICS; AIRCRAFT CONTROL; CLOSED LOOP CONTROL SYSTEMS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SOFTWARE; INTEGRATION; MEMORY ARCHITECTURE; TURNAROUND TIME;

AIRCRAFT;

EID: 84897681857     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. L. Fornasier, H. Rieger, U. Tremel, E. van der Weide, Time Dependent Aeroelastic Simulation of Rapid Manoeuvering Aircraft, AIAA 2002-0949, Reno 2002
2. ICEMCFD - Tetra/Prism Mesh-Generator
3. CENTAURSOFT, Centaur Mesh-Genera-tor
4. Transcendata CAD-repair system
5. L. Fornasier, F. Deister, O. Hassan, U. Tremel, Weatherhill: Robust and Efficient Generation of Unstructured Surface Grids about Geometrically Complex Configurations Using "Real-Design" CAD Data, AIAA 2003-805, Aerospace Sciences Conference 2003, Reno NV, 2003
6. F. Deister, U. Tremel, E. Hirschel, H. Rieger: Automatic Feature-Based Sampling of Native CAD Data for Surface Grid Generation, Notes on Numerical Fluid Mechanics, Springer Verlag, Berlin/ Heidelberg/New York, 2003
7. F. Deister, E.H. Hirschel: Self-Organizing Hybrid Cartesian Grid/Solution System with Multigrid, AIAA 2002-0112, Reno 2002