Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations / Stanley J. Osher.

Bibliographic Details
Uniform Title:	NASA contractor report ; NASA CR-174051.
Main Author:	Osher, Stanley
Corporate Authors:	Langley Research Center University of California (System). Regents
Language:	English
Published:	Hampton, Va. : NASA Langley Research Center, [1985]
Series:	NASA contractor report ; NASA CR-174051.
Subjects:	Aerodynamics, Supersonic.
Physical Description:	1 volume : illustrations ; 28 cm.
Format:	Government Document Microfilm Book

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