Complex Aeroengine Intake Ducts and Dynamic Distortion-Reference-Cited by-同舟云学术

Complex Aeroengine Intake Ducts and Dynamic Distortion

Published:2017-07 Issue:7 Volume:55 Page:2395-2409
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

MacManus David G.¹,Chiereghin Nicola¹,Prieto Daniel Gil¹,Zachos Pavlos¹

Affiliation:

1. Cranfield University, Bedfordshire, England MK43 0AL, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J054905

Reference35 articles.

1. “A Methodology for Assessing Inlet Swirl Distortion,” Soc. of Automotive Engineers Aerospace Information Rept. 5686, Warrendale, PA, 2007.

2. Encyclopedia of Aerospace Engineering;Bissinger N. C.,2010

3. MitchellG. A. “Effect of Inlet Ingestion of a Wing Tip Vortex on Compressor Face Flow and Turbojet Stall Margin,” NASA TM X-3246, 1975.

4. MitchellG. A. “Effect of Inlet Ingestion of a Wing Tip Vortex on Turbojet Stall Margin,” NASA TM-X-71610, 1974.

5. MeyerW.PazurW.FottnerL. “The Influence of Intake Swirl Distortion on the Steady-State Performance of a Low Bypass Twin-Spool Engine,” AGARD Rept. CP-498, 1991.

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