Analytical contouring of pintle nozzle exit cone using computational fluid dynamics-Reference-Cited by-同舟云学术

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Analytical contouring of pintle nozzle exit cone using computational fluid dynamics

Published:1995-07-10 Issue: Volume: Page:
ISSN:
Container-title:31st Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Smith-Kent Randall,Loh Hai-Tien,Chwalowski Pawel

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-2877

Reference11 articles.

1. Computation of viscous chemically reacting flows in hybrid rocket motors using an upwind LU-SSOR scheme

2. One- and Two-Phase Nozzle Flows

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3. Transient flow characteristics and performance of a solid rocket motor with a pintle valve;Chinese Journal of Aeronautics;2020-12

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