Some Studies of the Flow Pattern at the Base of Missiles with Rocket Exhaust Jets-Reference-Cited by-同舟云学术

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Some Studies of the Flow Pattern at the Base of Missiles with Rocket Exhaust Jets

Published:1960-06-01 Issue: Volume: Page:
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Author:

Goethert B. H.,Barnes L. T.

Publisher

Defense Technical Information Center

Cited by 13 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. Aeroacoustic Coupling Effect During the Ascent of Space Transportation Systems;AIAA Journal;2021-07

2. On subsonic near-wake flows of a space launcher configuration with various base geometries;Experiments in Fluids;2021-05-19

3. Three-dimensional simulation of rocket nozzles with multi-jet interaction using shock-unsteadiness model;AIAA Aviation 2019 Forum;2019-06-15

4. Twin Jet Interaction and Reverse Flow;Journal of Spacecraft and Rockets;2015-11

5. Supersonic wind tunnel simulation of propulsive jets;Journal of Spacecraft and Rockets;1985-09

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