The flow about the trailing edge of a supersonic oscillating aerofoil

DOI10.1017/S0022112075003138zbMath0316.76045OpenAlexW2036307918MaRDI QIDQ4077661

P. G. Daniels

Publication date: 1975

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112075003138

Mathematics Subject Classification ID

Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (10)

The viscous interaction between sound waves and the trailing edge of a supersonic splitter plate ⋮ Calculation of pressure in the linear problem of vibrator in a supersonic boundary layer ⋮ Biorthogonal Eigenfunction System in the Triple‐Deck Limit ⋮ Formation of recirculation zones in the boundary layer of a moving surface ⋮ Unsteady viscous supersonic flow over a short flap ⋮ On the unsteady three-dimensional boundary layer freely interacting with the external stream ⋮ Thermal waves in a supersonic boundary layer with self-induced pressure ⋮ Interaction between the boundary layer and a supersonic flow when part of the wall is rapidly heated ⋮ Interaction of an unsteady three-dimensional boundary layer with a hypersonic flow near a rapidly heated section of the surface ⋮ On the propagation of non-steady perturbations in a boundary layer with selfinduced pressure

Cites Work

• NUMERICAL AND ASYMPTOTIC SOLUTIONS FOR THE SUPERSONIC FLOW NEAR THE TRAILING EDGE OF A FLAT PLATE
• Self-induced separation
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• Linearized supersonic aerofoil theory part I
• On the Flow of an Incompressible Viscous Fluid Past a Flat Plate at Moderate Reynolds Numbers

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