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Numerical computation of viscous blunt body flows with a planar impinging shockTwo- and three-dimensional, viscous blunt body flows with planar impinging shocks are computed using an explicit, time-dependent, finite-difference method to solve the complete set of Navier-Stokes equations. The bow shock is treated as a discontinuity, while all interior shock layer detail such as shear layers, shock waves, jets and the wall boundary layer are automatically captured in the solution. Numerical results are presented for cases in which planar shock waves of different strengths and orientations are allowed to impinge on the flow field surroundings an infinite cylinder resulting in two- and three-dimensional shock interference patterns. The numerical results are compared with experiment.
Document ID
19750010439
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Holst, T. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Tannehill, J. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Rakich, J. V.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-X-70408
Report Number: NASA-TM-X-70408
Accession Number
75N18511
Funding Number(s)
CONTRACT_GRANT: NGR-16-002-038
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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