The effect of Mach number on the spatial stability of adiabatic flat plate flow to oblique disturbances

DOI10.1063/1.864630zbMath0543.76086OpenAlexW2073277153MaRDI QIDQ3332591

H. Taghavi, A. R. Wazzan, Gerlina Keltner

Publication date: 1984

Published in: The Physics of Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.864630

zbMATH Keywords

Mach numberspatial stabilityfinite difference techniquesoblique disturbancesadiabatic flat plate floweffect of Mach numberfrequency-Reynolds number diagram

Mathematics Subject Classification ID

Parallel shear flows in hydrodynamic stability (76E05) Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

Related Items (2)

Compressible boundary-layer stability theory ⋮ Dense-gas effects on compressible boundary-layer stability

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