Add to ORKGThe characteristics of flow oscillation induced by the interaction of weak normal shock wave with turbulent boundary layer in a supersonic nozzle are experimentally investigated and the ratio of the pressure fluctuations upstream and downstream of the interaction region is compared with the results of small disturbance theory. Spectral analyses of the pressure fluctuations are performed and the influences of the resonance on the oscillatory frequency of the shock are discussed
International audienceIn shock wave/boundary layer interactions, two mechanisms have been recognized...
International audienceIn shock wave/boundary layer interactions, two mechanisms have been recognized...
The experimental study of the effect of weak shock waves on the supersonic boundary layer of the fla...
The characteristics of flow field along spanwise direction induced by the interaction of weak normal...
An experimental investigation has been conducted to study the unsteady nature of the shock structure...
The flow in transonic diffusers and supersonic air intakes often becomes unsteady due to shock wave-...
The interaction between a weak normal shock wave and a turbulent boundary layer at free-stream Mach ...
The interaction of a spatially developing supersonic turbulent boundary layer with an impinging obli...
The interaction of a spatially developing supersonic turbulent boundary layer with a normal shock wa...
Shock wave / boundary layers interactions occur in wide-range of supersonic internal and external fl...
The need for better understanding of the low-frequency unsteadiness observed in shock wave/turbulent...
As part of the continuing technological advance towards the design of transonic steam turbine blades...
Pressure fluctuations due to the interaction of a shock wave with a turbulent boundary layer were in...
Abstract: The flow in transonic diffusers and supersonic air intakes often becomes unsteady due to s...
The experimental study of the effect of weak shock waves on the supersonic boundary layer of the fla...
International audienceIn shock wave/boundary layer interactions, two mechanisms have been recognized...
International audienceIn shock wave/boundary layer interactions, two mechanisms have been recognized...
The experimental study of the effect of weak shock waves on the supersonic boundary layer of the fla...
The characteristics of flow field along spanwise direction induced by the interaction of weak normal...
An experimental investigation has been conducted to study the unsteady nature of the shock structure...
The flow in transonic diffusers and supersonic air intakes often becomes unsteady due to shock wave-...
The interaction between a weak normal shock wave and a turbulent boundary layer at free-stream Mach ...
The interaction of a spatially developing supersonic turbulent boundary layer with an impinging obli...
The interaction of a spatially developing supersonic turbulent boundary layer with a normal shock wa...
Shock wave / boundary layers interactions occur in wide-range of supersonic internal and external fl...
The need for better understanding of the low-frequency unsteadiness observed in shock wave/turbulent...
As part of the continuing technological advance towards the design of transonic steam turbine blades...
Pressure fluctuations due to the interaction of a shock wave with a turbulent boundary layer were in...
Abstract: The flow in transonic diffusers and supersonic air intakes often becomes unsteady due to s...
The experimental study of the effect of weak shock waves on the supersonic boundary layer of the fla...
International audienceIn shock wave/boundary layer interactions, two mechanisms have been recognized...
International audienceIn shock wave/boundary layer interactions, two mechanisms have been recognized...
The experimental study of the effect of weak shock waves on the supersonic boundary layer of the fla...