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December 3, 2010 | History
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Publish Date
1995
Publisher
National Aeronautics and Space Administration, Langley Research Center,
Available from the National Technical Information Service
Language
English
Pages
214
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Subjects
Aerodynamics, Hypersonic, Air intakes, Airplanes, Computational fluid dynamics, Engine inlets, Flow distribution, Hypersonic Aerodynamics, Hypersonic speed, Inlet flow, Internal flow, Laminar boundary layer, Oblique shock waves, Pressure measurement, Ramjet engines, Scramjet engines, Shock wave interaction, Supersonic combustion ramjet engines, Three dimensional flow, Wind tunnel testsShowing 2 featured editions. View all 2 editions?
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1
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
1995, National Aeronautics and Space Administration, Langley Research Center, Available from the National Technical Information Service
Microform
in English
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2
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
1995, National Aeronautics and Space Administration, Langley Research Center, Available from the National Technical Information Service
in English
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Book Details
Edition Notes
"September 1995."
"Performing organization report number L-17349"--Report documentation page.
Includes bibliographical references (p. 10-11).
Available electronically at the following URL address: http://techreports.larc.nasa.gov/ltrs/ltrs.html.
Performed by Langley Research Center for the National Aeronautics and Space Administration WU 506-40-41-02.
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Feedback?December 3, 2010 | Edited by Open Library Bot | Added subjects from MARC records. |
January 19, 2010 | Edited by WorkBot | add subjects and covers |
December 11, 2009 | Created by WorkBot | add works page |