An adaptive grid method for computing the high speed 3D viscous flow about a re-entry vehicle
An adaptive grid method for computing the high speed 3D viscous flow about a re-entry vehicle
- Neue Suche nach: Bockelie, Michael J.
- Neue Suche nach: Smith, Robert E.
- Neue Suche nach: Bockelie, Michael J.
- Neue Suche nach: Smith, Robert E.
An algebraic solution adaptive grid generation method that allows adapting the grid in all three coordinate directions is presented. Techniques are described that maintain the integrity of the original vehicle definition for grid point movement on the vehicle surface and that avoid grid cross over in the boundary layer portion of the grid lying next to the vehicle surface. The adaptive method is tested by computing the Mach 6 hypersonic three dimensional viscous flow about a proposed Martian entry vehicle.
Dokumentinformationen
An adaptive grid method for computing the high speed 3D viscous flow about a re-entry vehicle
AIAA Applied Aerodynamics Conference ; 1992 ; Palo Alto, CA, United States
1992-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
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