Flow features of shock-induced combustion around projectile travelling at hypervelocities
31st Aerospace Sciences Meeting ; 1993 ; Reno , NV , U.S.A.
01.01.1993
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flow Features of Shock-lnduced Combustion Around Projectile Traveling at Hypervelocities
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