Base heating scaling criteria for a four- engine rocket cluster operating at high altitude
Author:
Affiliation:
1. CORNELL AERONAUTICAL LAB., INC., BUFFALO, N.Y.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1965-826
Reference27 articles.
1. BASE HEATING ON A MULTIPLE PROPULSION NOZZLE MISSILE
Cited by 7 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. Scaled Rocket Testing in Hypersonic Flow;20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;2015-07-02
2. Aft End Heating Assessment of Multiple Engine Clusters for a Reusable First Stage Launch Vehicle;AIAA SPACE 2012 Conference & Exposition;2012-09-11
3. Grid-Resolved Analysis of Base Flowfield for Four-Engine Clustered Nozzle Configuration;Journal of Spacecraft and Rockets;1996-01
4. A solution-adaptive gridding analysis of base flowfield for a four-engine clustered nozzle configuration;6th Joint Thermophysics and Heat Transfer Conference;1994-06-20
5. Development of a hot rocket subscale Space Shuttle model for base flow studies;10th Propulsion Conference;1974-08-16
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