Numerical simulation of unsteady flow in liquid propellant rocket engine with PISO algorithm-Reference-Cited by-同舟云学术

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Numerical simulation of unsteady flow in liquid propellant rocket engine with PISO algorithm

Published:1996-07-01 Issue: Volume: Page:
ISSN:
Container-title:32nd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Liu Weidong¹,Wang Zhenguo¹,Zhou Jin¹,Zhuang Fengchen¹

Affiliation:

1. National Univ. of Defense Technology, Changsha, China

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3124

Reference16 articles.

1. [I] Chen, C.P.,Kim, Y.M., MAST:AComputerCodeforMultiphaseAll-SpeedTransient Flows in ComplexGeometries,NASA-CR-NAG8-092,1991.

2. Patankar,S.V.,NumericalMethodfor Heat Transfer and FluidFlow, 1981.

3. Issa,F_L,TheComputationofCompressibleRecirculatingFlowsbyaNon-IterationImplicit Scheme,J. compt.Phys.,Vpl:62,pp 66-82,1985

4. Issa,R.I,SolutionoftheImplicitDiscretized Fluid Flow EquationsbyOperator-Spliting J.Compt. Phys.,Vol:62,pp 40-65,1985.

5. Issa,RJ., SolutionoftheImplicitDiscretized ReactingFlowEquationsbyOperator-Spliting J. Compt.Phys.,Vol:62,pp 40-65,1985.

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1. The Model of Combustion Instability;Internal Combustion Processes of Liquid Rocket Engines;2016-05-20

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