Flowfield computations over the space shuttle Orbiter with a proposed canard at a Mach number of 5.8 and 50 degrees angle of attack

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93Jun_Reuter.pdf (1.81 MB)
Authors
Reuter, William H., IV
Subjects
Space shuttle
CFD
Canard
Hypersonic aerodynamics
Computational fluid dynamics
Advisors
Howard, Richard M.
Hobson, Garth V.
Buning, Pieter G.
Date of Issue
1993-06
Date
June 1993
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
Type
Thesis
Description
URI
https://hdl.handle.net/10945/39837
Series/Report No
Department
Aeronautical and Astronautical Engineering
Organization
Naval Postgraduate School (U.S.)
Identifiers
NPS Report Number
Sponsors
Funder
Format
39 p.
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
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