Three-Dimensional Supersonic Minimum Length Nozzle Design at High Temperature for Arbitrary Exit Cross Section-Reference-Cited by-同舟云学术

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Three-Dimensional Supersonic Minimum Length Nozzle Design at High Temperature for Arbitrary Exit Cross Section

Published:2014-10-10 Issue:11 Volume:39 Page:8233-8245
ISSN:1319-8025
Container-title:Arabian Journal for Science and Engineering
language:en
Short-container-title:Arab J Sci Eng

Author:

Abada Omar,Zebbiche Toufik,Abdallah El-Hirtsi Ahmed

Publisher

Springer Science and Business Media LLC

Subject

Multidisciplinary

Link

http://link.springer.com/content/pdf/10.1007/s13369-014-1377-z.pdf

Reference22 articles.

1. Anderson J.D. Jr: Fundamentals of Aerodynamics. McGraw-Hill, New York (1988)

2. Anderson J.D. Jr: Modern Compressible Flow: With Historical Perspective. McGraw-Hill, New York (1982)

3. Sutton, G.P.: Rocket Propulsion Elements, 6th edn. California (1992)

4. Sauer, R.: Method of Characteristics for Three Dimensional Axially Symmetrical Supersonic Flows. NACA TM-1133 (1947)

5. Strom, C.R.: The Method of Characteristics for Three Dimensional Real Gas Flows. Air Force Systems Command, AFFDL-TR-67-47 (1967)

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