Effect of Side Gust on Performance of External Compression Supersonic Inlet-Reference-Cited by-同舟云学术

Effect of Side Gust on Performance of External Compression Supersonic Inlet

Published:2019-03 Issue:2 Volume:56 Page:569-582
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Halwas Hussein K.¹,Aggarwal Suresh¹

Affiliation:

1. University of Illinois at Chicago, Chicago, Illinois 60607

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035093

Reference41 articles.

1. OswatitschK. “Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (The Efficiencies of Shock Diffusers),” NACA TM-1140, 1947 (in German).

2. FerriA.NucciL. M. “Preliminary Investigation of a New Type of Supersonic Inlets,” NACA Rept. 1104, 1951.

3. KantrowitzA.DonaldsonC. D. “Preliminary Investigation of Supersonic Diffusers,” NACA ACR-L5D20, 1945.

4. Intake Aerodynamics, Second Edition

5. AIAA Educational Series;Mahoney J. J.,1990

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