Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations
By: Stanley J. Osher
Contributors: Langley Research Center; University of California (System). Regents
Series: NASA-CR -- 174051; NASA contractor report -- 174051
Publisher: NASA Langley Research Center
Published: 1985
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Supersonic
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