Gas phase ignition of a solid fuel containing an oxidizer
Author:
Affiliation:
1. WATERLOO, U., WATERLOO, ONTARIO, CANADA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1968-496
Reference11 articles.
1. ARS series on Prowess in Astronautics and Rocketry (Academic Press;McAlevy R.F.,1960
2. Progress in Astronautics and Rocketry (Academic Press;Studies,1960
3. Preprint 63-514 (December, 1963). 6) Hermance, C.E., Shinnar, R., and Summerfield,M.
Cited by 3 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. Ignition of Homogeneous Solid Propellants under Shock Tube Conditions: Further Theoretical Development;AIAA Journal;1971-08
2. Gas phase ignition theory for homogeneous propellants under shock tube conditions;AIAA Journal;1970-09
3. Ignition of homogeneous solid propellants under shock tube conditions - Further theoretical developments;8th Aerospace Sciences Meeting;1970-01-19
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