Grid generation of a high-fidelity complex multibody Space Shuttle mated vehicle

Author:

DOMINIK D.1,WISNESKI J.1,RAJAGOPAL K.1,VUONG S.1,SIKORA J.1

Affiliation:

1. Rockwell International Corp., Space Systems Div., Downey, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. RamakrishnanS.V., C.L. ChenandD.F. Dominik.Scale E&% ontheFlowPasttheMaledspaceShuuleConfiguration, AIAA paper 92-2680(1992). RocketPlumeanditsEffect ontheMatedShuttle Conjiguration AIM paper 92-2612(1992).

2. Rajagopal K., K.Y. Szema, S.V. Ramakrishnan, CL. Chen and W. Lick, A Versatile Multi-Zonal Gridding Technique for Complex Geometries, AIAA paper 90-0011

3. Dominik D.F., K. Rajagopal,S.Vuong,J. Wisneski,C. Olling,G. Hock,andJ. Sikora.Navier-StokesSolution for the Space Shurtie VehicleUsing a Full-Scale High Fidelity Grid Model, AIAA paper 93-0419(1993). Fig.1. MatedSpaceShwtleCoiyigwniion.

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1. Computational Analyses of Complex Flows for Realistic Reusable Launch and Reentry Vehicles;34th AIAA Fluid Dynamics Conference and Exhibit;2004-06-19

2. Vortex Interaction with an Aerofoil Using Chimera and the AMR Algorithm;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2002-06-25

3. Navier-Stokes solution for the Space Shuttle vehicle using a full-scale high fidelity grid model;31st Aerospace Sciences Meeting;1993-01-11

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