Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle-Reference-Cited by-同舟云学术

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Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle

Published:2003 Issue:1-4 Volume:71 Page:161-181
ISSN:1386-6184
Container-title:Flow, Turbulence and Combustion (formerly Applied Scientific Research)
language:en
Short-container-title:Flow, Turbulence and Combustion

Author:

Nguyen Anh Thi,Deniau H.,Girard S.,Alziary de Roquefort T.

Publisher

Springer Science and Business Media LLC

Subject

Physical and Theoretical Chemistry,General Physics and Astronomy,General Chemical Engineering

Cited by 66 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

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