Optimization of Blade Sweep in a Transonic Axial Compressor Rotor-Reference-Cited by-同舟云学术

Optimization of Blade Sweep in a Transonic Axial Compressor Rotor

Published:2005 Issue:4 Volume:48 Page:793-801
ISSN:1340-8054
Container-title:JSME International Journal Series B
language:en
Short-container-title:JSME international journal. Ser. B, Fluids and thermal engineering

Author:

JANG Choon-Man¹,LI Ping²,KIM Kwang-Yong²

Affiliation:

1. Fire & Engineering Services Research Department, Korea Institute of Construction Technology

2. Department of Mechanical Engineering, Inha University

Publisher

Japan Society of Mechanical Engineers

Subject

Fluid Flow and Transfer Processes,Physical and Theoretical Chemistry,Mechanical Engineering

Link

http://www.jstage.jst.go.jp/article/jsmeb/48/4/48_4_793/_pdf

Reference18 articles.

1. (1) Suder, K.L. and Celestina, K.L., Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor, ASME Paper 94-GT-365, (1994).

2. (2) Hah, C., Rabe, D.C. and Wadia A.R., Role of Tip Leakage Vortices and Passage Shock in Stall Inception in a Sweep Transonic Compressor Rotor, ASME GT2004-53867.

3. Calculation of Tip Clearance Effects in a Transonic Compressor Rotor

4. (4) Xu, C. and Amano, R.S., Numerical Prediction of Swept Blade Aerodynamic Effects, Proc. of ASME Turbo Expo 2004, ASME GT2004-53008.

5. (5) Bliss, D.B., Method and Apparatus for Preventing Leading Edge Shock Related Noise in Transonic and Supersonic Blades and Like, US Patent 3989406, (1976).

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