Mach Disk from Underexpanded Axisymmetric Nozzle Flow-Reference-Cited by-同舟云学术

Mach Disk from Underexpanded Axisymmetric Nozzle Flow

Published:1974-08 Issue:8 Volume:12 Page:1079-1082
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

CHANG I.SHIH¹,CHOW W. L.¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.49415

Reference16 articles.

1. Chang, I.S. "Mach Reflection, Mach Disk, and the Associated Nozzle Free Jet Flows," Ph.D. thesis,1973, Dept. of Mechanical and Industrial Engineering,Univ. of Illinoisat Urbana-Champaign, Urbana, 111.

2. Interferometric Studies of Faster than Sound Phenomena. Part II. Analysis of Supersonic Air Jets

3. Interferometric Studies of Faster than Sound Phenomena. Part II. Analysis of Supersonic Air Jets

4. On the Structure of Jets from Highly Underexpanded Nozzles Into Still Air

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