The Transonic Flow Field of an Axial Compressor Blade Row-Reference-Cited by-同舟云学术

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The Transonic Flow Field of an Axial Compressor Blade Row

Published:1958-10 Issue:10 Volume:25 Page:616-626
ISSN:1936-9999
Container-title:Journal of the Aerospace Sciences
language:en
Short-container-title:Journal of the Aerospace Sciences

Author:

McCUNE JAMES E.¹

Affiliation:

1. Cornell University,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.7813

Reference10 articles.

1. McCune, James E., The Three-Dimensional Flow Field of an Axial Compressor Blade Row-Subsonic, Transonic and Supersonic, Ph.D. Thesis,Cornell University, 1958. (See also AFOSR T N 58-72, ASTIA number AD 148 116 and 117.)

2. Olver, F . W. J., Philosophical Transactions of the Royal Society, Series A, No. 247, pp.307-368,1955.

Cited by 13 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. Theory of Blade Design for Large Deflections: Part II—Annular Cascades;Journal of Engineering for Gas Turbines and Power;1984-04-01

2. Theory of Blade Design for Large Deflections: Part I—Two-Dimensional Cascade;Journal of Engineering for Gas Turbines and Power;1984-04-01

3. Three-dimensional theory for the steady loading on an annular blade row;AIAA Journal;1981-04

4. Vorticity Modeling of Blade Wakes behind Isolated Annular Blade-Rows: Induced Disturbances in Swirling Flows;Journal of Engineering for Power;1981-04-01

5. Linearized analysis of the three-dimensional compressible flow through a rotating annular blade row;Journal of Fluid Mechanics;1981-02

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