Flow-structural interaction inside a solid rocket during ignition transient
Author:
Affiliation:
1. Aerospace Corp., El Segundo, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3286
Reference11 articles.
1. Internal ballistics of slotted-tube, solid- propellant rocket motors.
2. Segmented solid rocket motor internal flow simulations
3. High resolution schemes for hyperbolic conservation laws
4. A high-resolution TVD finite volume scheme for the Euler equations in conservation form
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. Detailed Simulations of Propellant Slumping in the TitanIV SRMU PQM-1;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09
2. Coupled transient flowfield and propellant deformation analysis for the Titan IV 7-segment solid rocket motor;30th Joint Propulsion Conference and Exhibit;1994-06-27
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