Results 91 to 100 of about 140,231 (211)

Experimental study of two separating turbulent boundary layers [PDF]

open access: yes
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
core   +1 more source

Relaxation of an unsteady turbulent boundary layer on a flat plate in an expansion tube [PDF]

open access: yes
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]

open access: yesFlow Turbul Combust, 2017
Vinuesa R   +4 more
europepmc   +1 more source

Flow separation in shock wave boundary layer interactions at hypersonic speeds [PDF]

open access: yes
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.
core   +1 more source

Revisiting History Effects in Adverse-Pressure-Gradient Turbulent Boundary Layers. [PDF]

open access: yesFlow Turbul Combust, 2017
Vinuesa R   +5 more
europepmc   +1 more source

An experimental study of the properties of surface pressure fluctuations for separating turbulent boundary layers [PDF]

open access: yes
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.
core   +1 more source

Adverse-Pressure-Gradient Effects on Turbulent Boundary Layers: Statistics and Flow-Field Organization. [PDF]

open access: yesFlow Turbul Combust, 2017
Sanmiguel Vila C   +5 more
europepmc   +1 more source

Vorticity interaction effects on blunt bodies [PDF]

open access: yes
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.
core   +1 more source

Home - About - Disclaimer - Privacy