NASA NTRS · 19930090967
On Reflection of Shock Waves from Boundary Layers
Abstract
Measurements are presented at Mach numbers from about 1.3 to 1.5 of reflection characteristics and the relative upstream influence of shock waves impinging on a flat surface with both laminar and turbulent boundary layers. The difference between impulse and step waves is discussed and their interaction with the boundary layer is compared. General considerations on the experimental production of shock waves from wedges and cones and examples of reflection of shock waves from supersonic shear layers are also presented.
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Liepmann, H W, Roshko, A, Dhawan, S. 1952-01-01. On Reflection of Shock Waves from Boundary Layers. https://ntrs.nasa.gov/citations/19930090967
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