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Simulation of High-Enthalpy Turbulent Shock Wave/Boundary Layer Interaction Using a RANS Approach
In the era of space exploration, the scientific community is strongly focusing on the analysis of hypersonic flows in the presence of shock...
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Flow structures and unsteadiness in hypersonic shock wave/turbulent boundary layer interaction subject to steady jet
Direct numerical simulations of Mach 6 hypersonic flow over a 34° compression corner subject to steady jet are conducted. Distributions of skin...
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Swept shock/boundary-layer interaction control using micro-vortex generators
Passive flow control devices, such as vortex generators (VGs), have shown to be successful in controlling flows associated with...
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Porous Bleed Boundary Conditions for Supersonic Flows With & Without Shock-Boundary Layer Interaction
This paper aims to evaluate the prediction accuracy of various porous bleed models on two flow cases of particular interest for supersonic...
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Visualization study of perturbations induced by plasma actuators and its effect on shock wave/boundary-layer interaction
AbstractSurface arc plasma actuator array is used to control the shock wave/boundary-layer interaction in a Ma = 2 flow. Two types of interaction are...
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Effects of Flow Pulsation on Shock Wave/Boundary Layer Interaction in Supersonic Isolator
In scramjet engine, inlet isolator is used to provide stable compressed flow to the combustors. A series of oblique shocks are used to compress the...
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Numerical Simulation of Shock Wave Turbulent Boundary Layer Interaction over Flat Plate at Mach 6
Numerical simulations of the unsteady compressible Navier–Stokes are carried out for shock wave turbulent boundary layer interaction (SWTBLI) at...
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Flow Control Using MVG in Shock Wave/Boundary Layer Interaction
This review study mainly focusses on micro vortex generator (MVG) as a flow control device for shock wave/boundary layer interaction. The flow...
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Crossflow effects on shock wave/turbulent boundary layer interactions
The effects of crossflow on the interaction between an im**ing shock wave and a high-speed turbulent boundary layer are investigated using direct...
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On the investigation of shock wave/boundary layer interaction with a high-order scheme based on lattice Boltzmann flux solver
Shock wave/boundary layer interaction (SWBLI) continues to pose a significant challenge in the field of aerospace engineering. This paper aims to...
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Relationship between secondary separation and surface pressure structure in swept shock-wave/boundary-layer interaction
A theoretical analysis is presented to elucidate the relationship between the skin friction topology of the secondary separation bubble and surface...
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Numerical studies on uncontrolled and controlled shock wave/boundary layer interactions in hypersonic intake
Understanding the phenomenon of Shock Wave/Boundary Layer Interaction (SBLI) is critical in develo** hypersonic aircraft as it is associated with...
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Asymmetry of a Flow Which is Due to the Interaction of a Compression Shock with the Boundary Layer on a Longitudinally Ribbed Surface
Numerical investigations of the asymmetry of a fluid flow in the channel of an air intake which is due to the interaction of a compression shock,...
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Multi-scale study of the transitional shock-wave boundary layer interaction in hypersonic flow
A high-fidelity simulation of the massively separated shock/transitional boundary layer interaction caused by a 15-degrees axisymmetrical compression...
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Mach number effects on shock-boundary layer interactions over curved surfaces of supersonic turbine cascades
The effects of inlet Mach number on the unsteadiness of shock-boundary layer interactions (SBLIs) over curved surfaces are investigated for a...
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Shock–shock interaction on the Reusability Flight Experiment (ReFEx)
The Reusability Flight Experiment (ReFEx) is currently under development at the German Aerospace Center (DLR). A coupled experimental and numerical...
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Hybrid LES/RANS Simulation of Shock/Turbulent Boundary-Layer Interactions
In order to reduce the computational cost of Large Eddy Simulation method at high Reynolds number, the hybrid LES/RANS model-Improved Delayed...
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Vibration Reduction of a Compliant Panel Under Ramp-Induced Shock Wave/Boundary Layer Interaction Through Aeroelastic Tailoring
Experiments are performed in a Mach 2 wind tunnel to investigate the vibration of a compliant panel under a ramp-induced shock wave/boundary layer...
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Numerical studies on weak and strong ignition induced by reflected shock and boundary layer interaction
In shock tube experiments, the interaction between the reflected shock and boundary layer can induce shock bifurcation and weak ignition. The weak...
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Nozzle geometry effects on supersonic wind tunnel studies of shock–boundary-layer interactions
Many supersonic wind tunnel experiments investigate shock–boundary-layer interactions by measuring the response of tunnel wall boundary layers to an...
