Compressor blade row unsteady aerodynamic response to attached and separated flow forcing functions
30th Aerospace Sciences Meeting and Exhibit ; 1992 ; Reno , NV , U.S.A.
01.01.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Axial Compressor Blade-to-Blade Unsteady Aerodynamic Variability
Online Contents | 2003
|Separated flow unsteady aerodynamic theory
AIAA | 1985
|