3-D Coupled Simulations of Flexible Inhibitors in the RSRM-Reference-Cited by-同舟云学术

3-D Coupled Simulations of Flexible Inhibitors in the RSRM

Published:2005-07-10 Issue: Volume: Page:
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Container-title:41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Wasistho Bono,Fiedler Robert,Namazifard Alireza,Brandyberry Mark

Publisher

American Institute of Aeronautics and Astronautics

Reference33 articles.

1. 1Gibby, H. "The Control of Ignition Transients Through Propellant Grain Inhibiting", AIAA Solid Propellant Rocket Conference, AIAA-1964-124, Jan.29-31,1964.

2. 2McWhorter, B. B. "Real-Time Inhibitor Recession Mesaurements in Two Space Shuttle Reusable Solid Rocket Motors", AIAA/ASME/SAE/ASEE JointPropulsion Conference andExhibit, AIAA-2003-5107, July 2-23,2003.

3. Vortex-shedding phenomena in solid rocket motors

4. Vortex driving mechanism in oscillatory rocket flows

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