Passive shock wave/boundary layer control of a helicopter rotor airfoil in a contoured transonic wind tunnel
25th AIAA Aerospace Sciences Meeting ; 1987 ; Reno , NV , U.S.A.
01.01.1987
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Study of Passive Control in a Transonic Shock Wave-Boundary-Layer Interaction
Online Contents | 1998
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