Attenuation of the shock in a shock tube due to the effect of wall boundary layer
6th Aerospace Sciences Meeting ; 1968 ; New York , NY , U.S.A.
01.01.1968
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Attenuation in shock tube due to unsteady-boundary-layer action
Engineering Index Backfile | 1956
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