返回Google圖書搜尋

Performance of Single-stage Axial-flow Transonic Compressor with Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and with Design Pressure Ratio of 2.05

Royce D. Moore

出版	National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
URL	http://books.google.com.hk/books?id=MeyGyEFMmVEC&hl=&source=gbs_api