Investigation of the Stall Hammershock at the Engine Inlet-Reference-Cited by-同舟云学术

Investigation of the Stall Hammershock at the Engine Inlet

Published:1975-04 Issue:4 Volume:12 Page:198-204
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Kurkov Anatole P.¹,Soeder Ronald H.¹,Moss John E.¹

Affiliation:

1. NASA Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.59818

Reference13 articles.

1. The flight investigation of pressure phenomena in the air intake of an F-111A airplane

2. Choby, D. A., Burstadt, P. L., and Calogeras, J. E. "Unstart and Stall Interactions Between a Turbojet Engine and an Axisymmetric Inlet with 60-Percent Internal-Area Contraction," TM X-2192,1971, NASA.

3. Prediction of Inlet Duct Overpressures Resulting from Engine Surge

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