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Ascent Aerodynamic Pressure Distributions on WB001To support the reusable launch vehicle concept study, the aerodynamic data and surface pressure for WB001 were predicted using three computational fluid dynamic (CFD) codes at several flow conditions between code to code and code to aerodynamic database as well as available experimental data. A set of particular solutions have been selected and recommended for use in preliminary conceptual designs. These computational fluid dynamic (CFD) results have also been provided to the structure group for wing loading analysis.
Document ID
19960029265
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Vu, B. (NASA Marshall Space Flight Center Huntsville, AL United States)
Ruf, J. (NASA Marshall Space Flight Center Huntsville, AL United States)
Canabal, F. (NASA Marshall Space Flight Center Huntsville, AL United States)
Brunty, J. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Publication Information
Publication: Thirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology
Subject Category
Aerodynamics
Accession Number
96N29761
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19960029254Collected WorksThirteenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology
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