An edition of Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations
(1985)
Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations
by Stanley Osher
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December 3, 2010 | History
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Supersonic Aerodynamics| Edition | Availability |
|---|---|
1
Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations
1985, NASA Langley Research Center
Microform
in /languages/eng
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Edition Notes
"The Regents of the University of California."
"N85-10913"--Microfiche header
"Grant number NAG1-270."
Bibliography: p. 5-6
Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1985. 1 microfiche ; 11 x 15 cm
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| December 3, 2010 | Edited by Open Library Bot | Added subjects from MARC records. |
| December 11, 2009 | Created by WorkBot | add works page |