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Performance of a Supersonic Compressor with Swept and Tilted Diffuser Blades

Arthur W. GoldsteinRalph L. Schacht

出版	National Advisory Committee for Aeronautics, 1955
URL	http://books.google.com.hk/books?id=qqvxxwEACAAJ&hl=&source=gbs_api

註釋

Report presenting testing of a supersonic mixed-flow compressor of large weight-flow capacity with a stator with swept and tilted blades was tested over a range of air tip speeds. As rotor speed increased, stage efficiency decreased continuously. Results regarding the overall compressor performance, flow fluctuations, and static-pressure distribution are provided.