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Numerical investigation of the impingement of an oblique shock on a flat plate
V. M.K. Sastri
Published in Springer-Verlag
1988
Volume: 23
   
Issue: 2
Pages: 123 - 125
Abstract
The unsteady, compressible Navier-Stokes equations in Reynolds-averaged variables are solved for a shock wave turbulent boundary layer interaction. For the free stream Mach number 3.7 and Reynolds number 8.202×106 computation is performed using MacCormack's explicit-implicit finite difference scheme with 42×42 grid points. It is found that the peak heating amplification correlation agrees well with computational results. © 1988 Springer-Verlag.
About the journal
JournalData powered by TypesetWärme- und Stoffübertragung
PublisherData powered by TypesetSpringer-Verlag
ISSN00429929
Open AccessNo
Concepts (6)
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    AERODYNAMICS - AERODYNAMIC HEATING
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    FLUID DYNAMICS
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    Heat transfer
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    IMPINGING SHOCK WAVES
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    OBLIQUE SHOCK WAVE
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    Shock waves