Design Considerations for Tip Clearance Sensitivity of Centrifugal Compressors in Aeroengines-Reference-Cited by-同舟云学术

Design Considerations for Tip Clearance Sensitivity of Centrifugal Compressors in Aeroengines

Published:2019-05 Issue:3 Volume:35 Page:666-668
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Lou Fangyuan¹,Fabian John C.¹,Key Nicole L.¹

Affiliation:

1. Purdue University, West Lafayette, Indiana 47907

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.B37100

Reference15 articles.

1. Der Radialkompressor

2. Die Kenngrößen der verschiedenen Radformen und ihre Anwendung

3. Small Turbomachinery Compressor and Fan Aerodynamics

4. KlassenH. A.WoodJ. R.SchumannL. F. “Experimental Performance of a 16.10-Centimeter-Tip-Diameter Sweptback Centrifugal Compressor Designed for a 6:1 Pressure Ratio,” NASA TM X-3552, 1977.

5. KlassenH. A.WoodJ. R.SchumannL. F. “Experimental Performance of a 13.65-Centimeter-Tip-Diameter Tandem-Bladed Sweptback Centrifugal Compressor Designed for a Pressure Ratio of 6,” NASA TP-1091, 1977.

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