Stagnation temperature effect on the supersonic axisymmetric minimum length nozzle design with application for air-Reference-Cited by-同舟云学术

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Stagnation temperature effect on the supersonic axisymmetric minimum length nozzle design with application for air

Published:2011-11 Issue:10 Volume:48 Page:1656-1675
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Zebbiche Toufik

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference24 articles.

1. Fundamentals of Aerodynamics;Anderson,1982

2. Modern Compressible Flow: With Historical Perspective;Anderson,1988

3. Comparison of Minimum Length Nozzles;Argrow;J. Fluid Eng.,1988

4. Berger, M. Géométrie: Convexes et Poly-topes, Polyèdres réguliers, aires et Volumes, Tome 3, Fernand Nathan, Paris, 1978.

5. Demidovitch, B., Maron, I. Eléments de calcul numérique, Edition MIR, Moscou, 1987.

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