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Stage Separation CFD Tool Development and EvaluationThis viewgraph presentation evaluates CFD (Computational Fluid Dynamics) tools for solving stage separation problems. The demonstration and validation of the tools is for a second generation RLV (Reusable Launch Vehicle) stage separation. The flow solvers are: Cart3D; Overflow/Overflow-D; Unic.
Document ID
20030000733
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Droege, Alan (NASA Marshall Space Flight Center Huntsville, AL United States)
Gomez, Reynaldo (NASA Johnson Space Center Houston, TX United States)
Wang, Ten-See (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 21, 2013
Publication Date
July 1, 2002
Publication Information
Publication: Twelfth Thermal and Fluids Analysis Workshop
Subject Category
Fluid Mechanics And Thermodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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