Comparison of Theoretical and Semi-Empirical Solutions for Dissipation Coefficient in a Low Reynolds Number Compressor Cascade-Reference-Cited by-同舟云学术

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Comparison of Theoretical and Semi-Empirical Solutions for Dissipation Coefficient in a Low Reynolds Number Compressor Cascade

Published:2015-06-18 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Fluid Dynamics Conference
language:
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Author:

Kok Foo¹,Myose Roy Y.¹,Hayashibara Shigeo²

Affiliation:

1. Wichita State University

2. Embry-Riddle Aeronautical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2015-2314

Reference25 articles.

1. 1Otis, C.E., 1991, Aircraft Gas Turbine Powerplants, IAP, Inc.: Casper, WY.

2. 2Hill, P.G. and Peterson, C.R., 1992, Mechanics and Thermodynamics of Propulsion, McGraw-Hill: N.Y.

3. 4Serovy, G.K., 1989, "Performance Prediction for Axial-Flow Compressor and Turbine Blading," Blading Design for Axial Turbomachines, AGARD LS-167.

4. The 1993 IGTI Scholar Lecture: Loss Mechanisms in Turbomachines

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Effects of the Reynolds Number on the Efficiency and Stall Mechanisms in a Three-stage Axial Compressor;Journal of Applied Fluid Mechanics;2024-06-01

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