VORSTREM - A simple and versatile 2D viscous solver for chamber flow in solid rocket motors-Reference-Cited by-同舟云学术

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VORSTREM - A simple and versatile 2D viscous solver for chamber flow in solid rocket motors

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Salita Mark¹

Affiliation:

1. TRW, Inc., Ogden, UT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2779

Reference17 articles.

1. Gas-dynamic flow in a spinning, coning solid rocket motor

2. Salita, M.'Calculation of Steady Viscous FlowPast Barriers (with Applicationto Mixing-BowlBlades and Port InhibitorStubs): Phase I", Thiokol memo 2814-84-M013, 1/79/84.

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 analysis of the turbulent flow and alumina particle trajectories in solid rocket motors;33rd Joint Propulsion Conference and Exhibit;1997-07-06

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