Inlet flow test calibration for a small axial compressor facility. I - Design and experimental results-Reference-Cited by-同舟云学术

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Inlet flow test calibration for a small axial compressor facility. I - Design and experimental results

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Miller D.¹,Prahst P.²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. NYMA, Inc., Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2690

Reference17 articles.

1. Steinke, R. J. "Design of 9.271-Pressure Ratio Five Stage Core Compressor and Overall Performance for FirstThree Stages,"NASA TP2597, May 1986.

2. Supercritical Cascades Using Complex Characteristics and Boundary-Layer Correction," AIAAJournal, Vol.22, No.7,July 1984,pp.950-956.

3. The design/analysis of flows through turbomachinery - A viscous/inviscid approach

Cited by 3 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. Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors;International Journal of Turbo & Jet-Engines;2022-12-26

2. Effect of the distribution of the upstream probe support on performance of compressor cascade;International Journal of Turbo & Jet-Engines;2022-11-04

3. Effect of the distribution of the upstream probe support on performance of compressor cascade;International Journal of Turbo & Jet-Engines;2022-11-04

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