Wedge Shock and Nozzle Exhaust Plume Interaction in a Supersonic Jet Flow-Reference-Cited by-同舟云学术

Wedge Shock and Nozzle Exhaust Plume Interaction in a Supersonic Jet Flow

Published:2017-01 Issue:1 Volume:54 Page:125-134
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Castner Raymond¹,Zaman Khairul¹,Fagan Amy¹,Heath Christopher¹

Affiliation:

1. NASA John H. Glenn Research Center, Cleveland, Ohio 44135

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C033623

Reference30 articles.

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2. Aerodynamic Design of Shaped Sonic Boom Demonstration Aircraft

3. PutnamL.CaponeF. “Experimental Determination of Equivalent Solid Bodies to Represent Jets Exhausting into a Mach 2.20 External Stream,” NASA Rept. TN-D-5553, 1969.

4. CastnerR. S. “Analysis of Plume Effects on Sonic Boom Signature for Isolated Nozzle Configurations,” NASA Rept. TM-2008-215414, June 2008;

5. Analysis of Plume Effects on Sonic Boom Signature for Isolated Nozzle Configurations

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