Cooling of the Vulcain Nozzle＇s Divergent Wall

Cooling of the Vulcain Nozzle＇s Divergent Wall

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作者 Nassir Chellou Maamar Guendez Abdallah Benarous

机构地区 Department of Mechanical Engineering LCEMSM (Laboratory of ControL Tests

出处《Journal of Mechanics Engineering and Automation》 2015年第8期459-464,共6页 机械工程与自动化（英文版）

关键词冷却壁喷嘴发散 SolidWorks 发动机喷管 FLUENT 燃烧气体 ANSYS Propulsive nozzle, fluidic injection, heat fluxes.

参考文献8

1Guendez, M., Chellou, N., and Benarous~ A. 2014. "Flow Analysis in a Propulsive Nozzle Subjected to a Fluidic Injection." Presented at CIEP'I4, Constantine.
2Zmijanovic, V., Lago, V., Sellam, M., and Chpoun, A. 2014. "Thrust Shock Vector Control of an Axisymmetric Conical Supersonic Nozzle via Secondary Transverse GasInjection." Shock Wave 24 (1): 97-111.
3Haggander, J. 2001. An efficient Concept-Design Process for the Vulcain2 Thruster, Rapport Technique Volvo-Aero No. 102: Trollhatan, Sweden.
4JANAF. 1975. Rocket engine performance prediction and evaluation, CPIA Publication No. 246.
5DASSAULT SYSTEMS, Solidworks help, Simulationbackground.
6SOLIDWORKS customer software support.
7Guendez, M. 2014. "Analysis of the Film Cooling for a Propulsive Nozzle." Master II Project in Mechanical Engineering, University of Hassiba Benbouali, Chlef, Algeria.
8http://www.engineeringtoolbox.com/.

2015年第8期

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