Experimental Investigation of the Starting Behavior of a Three-Dimensional Scramjet Intake-Reference-Cited by-同舟云学术

Experimental Investigation of the Starting Behavior of a Three-Dimensional Scramjet Intake

Published:2015-09 Issue:9 Volume:53 Page:2686-2693
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Flock Andreas K.¹,Gülhan Ali¹

Affiliation:

1. Supersonic and Hypersonic Technology Department, DLR, German Aerospace Center, 51147 Cologne, Germany

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053786

Reference25 articles.

1. Hypersonic Airbreathing Propulsion

2. HermannR., Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics, Minneapolis-Honeywell Regulator Co., Minneapolis, MN, 1956, pp. 33–53, Chap. 2.

3. OswatitschK. “Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds,” NACA TM-1140, 1944.

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

5. AndersonJ. D. J., Fundamentals of Aerodynamics, 4th ed., McGraw–Hill, New York, 2007, pp. 548–552, Chap. 8.

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