Mach Reflection Associated with Over-Expanded Nozzle Free Jet Flows-Reference-Cited by-同舟云学术

Mach Reflection Associated with Over-Expanded Nozzle Free Jet Flows

Published:1975-06 Issue:6 Volume:13 Page:762-766
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

CHOW W. L.¹,CHANG I. S.²

Affiliation:

1. University of Illinois of Urbana-Champaign, Urbana, III.

2. Lockheed Missiles and Space Co., Huntsville, Ala.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.60434

Reference15 articles.

1. Chang, I. S. "Mach Reflection, Mach Disc, and the Associated Nozzle Free Jet Flows," Ph.D. thesis,1973, Dept. of Mechanical and Industrial Engineering, Universityof Illinois at Urbana-Champaign, Urbana, 111.; available from University MicroFilm Service, Ann Arbor, Mich, Micro No. 74-11973.

2. Interaction of Shock Waves

3. Interaction between primary and secondary streams of supersonic ejector systems and their performance characteristics

4. Calculations of axisymmetric jet leaving a nozzle at jet pressure lower than pressure in medium

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