An experimental research program providing basic knowledge and establishing a database on the fluctuating pressure loads produced on aerodynamic surfaces beneath 3D shock wave/boundary layer interactions is presented. A turbulent boundary layer on a flat plate is subjected to interactions with swept planar shock waves generated by sharp fins at angle of attack. Measurements are made for the first time in the aft areas of these interactions, showing fluctuating pressure levels as high as 160 dB.
Wall pressure fluctuations beneath swept shock wave/boundary layer interactions
AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States
1993-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Unsteady Pressure Loads Generated by Swept-Shock-Wave-Boundary-Layer Interactions
Online Contents | 1996
|Active control of swept shock wave-turbulent boundary-layer interactions
Online Contents | 2004
|