6 research outputs found
Unsteadiness Characterization in a Shock Wave Turbulent Boundary Layer Interaction through Dual-PIV
Aerospace Engineerin
Characterization of flow unsteadiness in a shock wave turbulent boundary layer interaction by means of dual-PIV
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Application of a dual-plane particle image velocimetry (dual-PIV) technique for the unsteadiness characterization of a shock wave turbulent boundary layer interaction
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Evaluation of integral forces and pressure fields from planar velocimetry data for incompressible and compressible flows
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