Plume Interaction in Parallel Multi-Thrusters Propulsion System and the Effect on Backflow-Reference-Cited by-同舟云学术

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Plume Interaction in Parallel Multi-Thrusters Propulsion System and the Effect on Backflow

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
language:
Short-container-title:

Author:

Xiao Ze-Juan¹,Cheng Hui-Er¹,Zhou Hong-Ling²

Affiliation:

1. Dept. of Aeronautics and Astronautics, Shanghai Jiao Tong University

2. Shanghai Institute of Space Propulsion

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3599

Reference9 articles.

1. I. E. Wrisdale, D. F. Mikulskis and M. R.Gilmore. Navier Stokes Calculations of a Twin Nozzle rocket Plume.AIAAPaper 96-1881

2. Analysis of Flowfields over Four-Engine DC-X Rockets

3. Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology

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. Plume influence analysis of small bipropellant thruster on solar array of GEO satellite;PLOS ONE;2018-09-04

2. Comparison study of exhaust plume impingement effects of small mono- and bipropellant thrusters using parallelized DSMC method;PLOS ONE;2017-06-21

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