IGTC-47 / ASME-83-GTJ-19 DESIGN AND PERFORMANCE COMPARISON OF THREE HIGH-SPEED FANS(Session B-2 Aerodynamics II (Turbomachinery))
スポンサーリンク
概要
- 論文の詳細を見る
A long-term research program for the years 1967-1981 was carried out to design and test high-speed, high-pressure-ratio scale model fans with booster stages. This paper summarizes the aerodynamic aspects of the program, with special reference to the design concepts and experimental results. A streamline curvature technique was used. Our fan research was directed towards increasing the inlet tip relative velocity up to Mach 1.4. Multiple- and double-circular-arc blade profiles were employed. We also discuss the flow separation due to the presence of swept blade rows.
- 公益社団法人日本ガスタービン学会の論文
著者
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Gomi M.
National Aerospace Laboratory
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Fujii S.
National Aerospace Laboratory
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Nishiwaki H.
National Aerospace Laboratory
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