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Application of Chimera Navier-Stokes Code for High Speed FlowsThe primary task for this year was performed in support of the "Trailblazer" project. The purpose of the task was to perform an extensive CFD study of the shock boundary-layer interaction between the engine-diverters and the primary body surfaces of the Trailblazer vehicle. Information gathered from this study would be used to determine the effectiveness of the diverters in preventing the boundary-layer coming off of the vehicle forebody from entering the main engines. The PEGSUS code was used to define the "holes" and "boundaries" for each grid. Two sets of CFD calculations were performed.Extensive post-processing of the results was performed.
Document ID
19980214884
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ajmani, Kumud
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA/CR-1997-207809
NAS 1.26:207809
Report Number: NASA/CR-1997-207809
Report Number: NAS 1.26:207809
Funding Number(s)
CONTRACT_GRANT: NCC3-550
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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