Flow features of shock-induced combustion around projectile travelling at hypervelocities
31st Aerospace Sciences Meeting ; 1993 ; Reno , NV , U.S.A.
1993-01-01
Conference paper
Electronic Resource
English
Flow Features of Shock-lnduced Combustion Around Projectile Traveling at Hypervelocities
Online Contents | 1995
|Research frontiers at hypervelocities. II.
NTRS | 1967
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Engineering Index Backfile | 1967
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Tema Archive | 1995
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