Computational Assessment of Gaseous Reacting Flows in Single Element Injector
Author:
Affiliation:
1. University of Michigan
2. Iowa State University
3. University of Florida
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-449
Reference30 articles.
1. 1Foust,M.J.,Deshpande,M.,Pal,S.,Ni,T.,Merkle,C.L.,Santoro,R.J."Experimentalandanalyticalcharacterizationofa shear coaxial combusting GO2/GH2flowfield,"AIAA-96-0646,34thAIAAAerospaceSciencesMeetingandExhibit,Jan15-18,Reno, NV, 1996
2. Comparison of computational codes for modeling hydrogen-oxygen injectors
3. Compressible and incompressible flow computations with a pressure based method
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