Rotor wake segment influence on stator-surface boundary layer development in an axial-flow compressor stage
23rd Joint Propulsion Conference ; 1987 ; San Diego , CA , U.S.A.
01.01.1987
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
An experimental study of rotor-stator wake unsteadiness in a multistage axial compressor
SAGE Publications | 2021
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