Fully Expanded Supersonic Flow Inside Conical and Contour Nozzle-Reference-Cited by-同舟云学术

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Fully Expanded Supersonic Flow Inside Conical and Contour Nozzle

Published:2012-03 Issue:2 Volume:49 Page:422-424
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Mehta R. C.¹,Natarajan G.¹,Bose N.²

Affiliation:

1. Noorul Islam University, Kumaracoil, Thuckalay 629 180, India

2. Mepco Schlenk Engineering College, Sivakasi 626 005, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32195

Reference11 articles.

1. Shapiro, A. H., The Dynamics and Thermodynamics of Fluid Flow, Ronald Press, New York, Vol.1, 1953, pp.74-78, 239.

2. Saad, M. A., Compressible Fluid Flow, Prentice-Hall, Upper SaddleRiver, NJ,1985, pp.95-99, 458-466.

3. Inviscid Laval-nozzle flowfield calculation

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical simulations of convergent-divergent nozzle and straight cylindrical supersonic diffuser;Advances in aircraft and spacecraft science;2014-10-25

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