Viscous Effects and Truncation Effects in Axisymmetric Busemann Scramjet Intakes-Reference-Cited by-同舟云学术

Viscous Effects and Truncation Effects in Axisymmetric Busemann Scramjet Intakes

Published:2016-06 Issue:6 Volume:54 Page:1881-1891
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Flock Andreas K.¹,Gülhan Ali¹

Affiliation:

1. 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.J054287

Reference31 articles.

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3. HermannR., Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics, Minneapolis-Honeywell Regulator Company, Minneapolis, MN, 1956, p. 255.

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

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