Direct Numerical Simulation Database for Hypersonic Turbulent Boundary Layers. [PDF]
Zhang C, Duan L, Choudhari MM.
europepmc +1 more source
Experimental study of two separating turbulent boundary layers [PDF]
A detailed study of two strong adverse pressure gradient flows, one with a free-stream velocity of 35 m/sec, at throat (producing a Re sub theta of 27000 at detachment) and another with free-stream velocity of 22 m/sec, at throat (producing a Re sub ...
Agarwal, N. K. +2 more
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Experimental Control of Turbulent Boundary Layers with In-plane Travelling Waves. [PDF]
Bird J, Santer M, Morrison JF.
europepmc +1 more source
Relaxation of an unsteady turbulent boundary layer on a flat plate in an expansion tube [PDF]
An analysis is presented for the relaxation of a turbulent boundary layer on a semi-infinite flat plate after passage of a shock wave and a trailing driver gas-driven gas interface. The problem has special application to expansion-tube flows.
Gurta, R. N., Trimpi, R. L.
core +1 more source
Pressure-Gradient Turbulent Boundary Layers Developing Around a Wing Section. [PDF]
Vinuesa R +4 more
europepmc +1 more source
Flow separation in shock wave boundary layer interactions at hypersonic speeds [PDF]
An assessment is presented for the experimental data on separated flow in shock wave turbulent boundary layer interactions at hypersonic and supersonic speeds.
Hamed, A.
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Revisiting History Effects in Adverse-Pressure-Gradient Turbulent Boundary Layers. [PDF]
Vinuesa R +5 more
europepmc +1 more source
An experimental study of the properties of surface pressure fluctuations for separating turbulent boundary layers [PDF]
Noise generated by helicopter and turbomachine rotors is a nuisance that designers would like to predict and to minimize within other design constraints.
Simpson, Roger L.
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Adverse-Pressure-Gradient Effects on Turbulent Boundary Layers: Statistics and Flow-Field Organization. [PDF]
Sanmiguel Vila C +5 more
europepmc +1 more source
Vorticity interaction effects on blunt bodies [PDF]
Numerical solutions of the viscous shock layer equations governing laminar and turbulent flows of a perfect gas and radiating and nonradiating mixtures of perfect gases in chemical equilibrium are presented for hypersonic flow over spherically blunted ...
Anderson, E. C., Wilcox, D. C.
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