Affiliation:
1. Marquette University
2. University of Tennessee Space Institute
Publisher
American Institute of Aeronautics and Astronautics
Reference62 articles.
1. Solid propellant acoustic admittance corrections
2. 2Flandro, G. A. "Nonlinear Combustion of a Solid Propellant with Velocity Coupling," AIAA Paper 83-1269,June1983.
3. Effects of vorticity on rocket combustion stability
4. 5Flandro, G. A. "On Flow Turning," AIAA Paper 95-2530,July1995.
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. Analytical and CFD Approximations for Tapered Slab Rocket Motors;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26