For abstract see AD B050 857L.
Investigation of a High-Through-Flow, Single-Stage Axial-Flow Compressor with Casing Vortex Generator Configuration 'B' (Configuration 1B)
1980
105 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Aircraft , Axial flow compressors , Vortex generators , Turbojet engines , Turbojet inlets , Axial flow compressor blades , Transonic flow , Compressor rotors , Tables(Data) , Computer printouts , Casing vortex generators , Single stage compressors , High through flow compressors , Rotor tips , S/L change 8312
Experimental Investigation of Circumferential Grooved Casing/Hub Treatment in Axial Flow Compressor
British Library Conference Proceedings | 1993
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