Influence study of flow separation on the nozzle vibration response-Reference-Cited by-同舟云学术

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Influence study of flow separation on the nozzle vibration response

Published:2016-06 Issue:2 Volume:5 Page:108-117
ISSN:2212-540X
Container-title:Propulsion and Power Research
language:en
Short-container-title:Propulsion and Power Research

Author:

Li Geng,Liu Qin,Han Xuequn,Guo Yunqiang

Funder

National Basic Research Development Program of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Fuel Technology,Aerospace Engineering,Automotive Engineering

Reference12 articles.

1. Nozzle flow separation;Hadjadj;Shock. Waves,2009

2. Shock pattern in the plume of rocket nozzles: needs for design consideration;Hagemann;Shock. Waves,2008

3. Flow separation side loads excitation of rocket nozzle FEM;Smalley,2007

4. J. Östlund, Flow processes in rocket engine nozzles with focus on flow separation and side-loads, Technical Report, 2002, 09.

5. M. Terhardt, G.I. Hagemann, M. Frey, Flow separation and side-load, Behaviok of the Vulcain engine AIAA 99-31448, 1999

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. Study on Separation Characteristics of Nozzles with Large Expansion Ratio of Solid Rocket Motors;Aerospace;2022-12-21

2. A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines;Combustion Theory and Modelling;2021-06-07

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