End-Wall Boundary Layers and Blockages of Multistage Axial Compressors Under Different Conditions-Reference-Cited by-同舟云学术

End-Wall Boundary Layers and Blockages of Multistage Axial Compressors Under Different Conditions

Published:2017-07 Issue:4 Volume:33 Page:908-916
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Zheng Xinqian¹,Yang Heli¹

Affiliation:

1. State Key Laboratory of Automotive Safety and Energy, Tsinghua University, 100084 Beijing, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B36251

Reference24 articles.

1. StratfordB. S. “The Use of Boundary Layer Techniques to Calculate the Blockage from the Annulus Wall Boundary Layer in a Compressor,” American Soc. of Mechanical Engineers Paper 67-WA/GT-7, Nov. 1967.

2. An Axial Compressor End-Wall Boundary Layer Theory

3. End-Wall Boundary Layers in Axial Compressors

4. An Axial Compressor End-Wall Boundary Layer Calculation Method

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