Calculation of pressure in the linear problem of vibrator in a supersonic boundary layer

DOI10.1016/0021-8928(79)90036-4zbMath0457.76049OpenAlexW1616775258MaRDI QIDQ1151302

E. D. Terent'ev

Publication date: 1979

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(79)90036-4

zbMATH Keywords

Fourier transformationexponential lawflow over vibrating triangular plate

Mathematics Subject Classification ID

Applications to the sciences (65Z05) Supersonic flows (76J20)

Related Items (7)

On forced oscillations in the boundary layer at frequencies near the upper branch of the neutral curve ⋮ Three-dimensional disturbances in a compressible boundary layer ⋮ On the linear problem of a supersonic flow of a viscous gas past a vibrator ⋮ Regions of existence of discrete spectral modes in a Blasius boundary layer ⋮ The linear problem of vibrator in a subsonic boundary layer ⋮ Thermal waves in a supersonic boundary layer with self-induced pressure ⋮ On the propagation of non-steady perturbations in a boundary layer with selfinduced pressure

Cites Work

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• On unsteady boundary layer with self-induced pressure
• The flow about the trailing edge of a supersonic oscillating aerofoil
• Upstream propagation of unsteady disturbances in supersonic boundary layers
• On the flow near the trailing edge of a flat plate II
• ON LAMINAR BOUNDARY LAYERS NEAR CORNERS
• On boundary layers and upstream influence. I. A comparison between subsonic and supersonic flows

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