Contribution of Downstream Stator to the Interaction Noise of a Single-Stage Axial-Flow Compressor
1967
20 pages
Report
Keine Angabe
Englisch
Aerodynamics , Jet & Gas Turbine Engines , Axial flow compressor , Noise reduction , Stator , Axial , Blade , Compressor , Downstream , Flow , Frequency , Guide , Inlet , Noise , Pattern , Radiation , Reduction , Rotor , Spectrum , Vane
British Library Online Contents | 1994
|Inlet noise studies for an axial-flow single-stage compressor
TIBKAT | 1965
|