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NASA/MSFC's Calculation for Test Case 1a of ATAC-FSDC Workshop on After-body and Nozzle FlowsMr. Ruf of NASA/MSFC executed the CHEM computational fluid dynamics (CFD) code to provide a prediction of the test case 1 a for the ATAC-FSDC Workshop on After-body and Nozzle Flows. CHEM is used extensively at MSFC for a wide variety of fluid dynamic problems. These problems include; injector element flows, nozzle flows, feed line flows, turbomachinery flows, solid rocket motor internal flows, plume vehicle flow interactions, etc.
Document ID
20070003682
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Ruf, Joseph H. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
November 16, 2006
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: ATAC-FSCD Workshop on Afterbody and Nozzle Flows
Location: Noordwijk
Country: Netherlands
Start Date: November 15, 2006
End Date: November 16, 2006
Sponsors: European Space Agency. European Space Research and Technology Center, ESTEC
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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