DC-X in-ground effect on base flow and heating environment
Author:
Affiliation:
1. NASA, Marshall Space Flight Center, Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2550
Reference27 articles.
1. Gielda, T.P., Walter, T.M., and Agarwal, R.K. "Single Stage Rocket Performance: Prediction and Test,"AIAAPaper 92-1386,March 1992.
2. Analysis of flowfields over four-engine DC-X rockets
3. Numerical analysis of base flowfield for a four-engine clustered nozzle configuration
4. Grid-Resolved Analysis of Base Flowfield for Four-Engine Clustered Nozzle Configuration
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. Numerical Study on the Flow Mechanism of Base Aerodynamic Force Acting on the Vertical Landing Rocket;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2006
2. GRASP - A general radiation simulation program;32nd Thermophysics Conference;1997-06-23
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