Influence of spatial discretization and unsteadiness on the simulation of rocket combustors-Reference-Cited by-同舟云学术

Influence of spatial discretization and unsteadiness on the simulation of rocket combustors

Published:2015-06-17 Issue:9 Volume:79 Page:437-455
ISSN:0271-2091
Container-title:International Journal for Numerical Methods in Fluids
language:en
Short-container-title:Int. J. Numer. Meth. Fluids

Author:

Lempke Markus¹,Keller Roman¹,Gerlinger Peter¹

Affiliation:

1. Institut für Verbrennungstechnik der Luft- und Raumfahrt; Universität Stuttgart; Pfaffenwaldring 38-40 70569 Stuttgart Germany

Funder

Deutsche Forschungsgemeinschaft

Publisher

Wiley

Subject

Applied Mathematics,Computer Science Applications,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/fld.4059/fullpdf

Reference40 articles.

1. Marshall WM Pal S Woodward RD Santoro RJ Benchmark wall heat flux data for a GO 2 /GH 2 single element combustor 41 st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Tucson, AZ 2005 3572

2. Locke JM Pal S Woodward RD Santoro RJ Toward time-resolved measurements in a gaseous hydrogen/oxygen rocket 45 th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Denver, CO 2009 5395

3. Pal S Marshall W Woodward R Santoro R Wall heat flux measurements for a uni-element GO 2 /GH 2 shear coaxial injector Third International Workshop on Rocket Combustion Modeling Vernon, France 2006

4. Locke JM Pal S Woodward RD Chamber wall heat flux measurements for a LOX/CH 4 uni-element rocket 43 rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit Cincinnati, OH 2007 5547

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