Shock tunnel investigation of boundary-layer transition at M equals 5.5
3rd and 4th Aerospace Sciences Meeting ; 1966 ; New York , NY , U.S.A.
01.01.1966
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Shock tunnel investigation of boundary-layer transition at M = 5.5
Engineering Index Backfile | 1967
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Engineering Index Backfile | 1954
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