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Cold-air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine
Jeffrey E. HaasMilton G. Kofskey
其他書名
Design and performance of a solid blade configuration. I
出版National Aeronautics and Space Administration, 1975
URLhttp://books.google.com.hk/books?id=_zJa6EG1kzwC&hl=&source=gbs_api
EBookFULL_PUBLIC_DOMAIN
註釋A solid blade version of a single-stage, axial-flow turbine was investigated to determine its performance over a range of speeds from 0 to 105 percent of equivalent design speed and over a range of total to static pressure ratios from 1.62 to 5.07.