Fluid flow in rocket nozzles-Reference-Cited by-同舟云学术

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Fluid flow in rocket nozzles

Published:1998-07-13 Issue: Volume: Page:
ISSN:
Container-title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Jones V.¹,Shukla K.¹

Affiliation:

1. ISRO, Vikram Sarabhai Space Centre, Trivandrum, India

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3840

Reference27 articles.

2. Applying the transformation defined by Eq.(7), hi the (C,r|)coordinate system,theEqs.(1-4) become :

3. The finite difference analogs for Eqs. (8-11) areasgiven below. For the predictor stepthese can bewritten respectively as:

4. '1-13I \ V"l V/ J \ 7"' V/ c(

Cited by 2 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. Performance Analysis of Thermal Protection System of a Solid Rocket Nozzle;Journal of Spacecraft and Rockets;2003-05

2. Performance Analysis of Thermal Protection System of a Solid Rocket Nozzle;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07

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