Visualization of hypersonic incident shock wave boundary layer interaction
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DOI: 10.1007/s12650-019-00622-0
Abstract: Abstract The incident shock interactions with the hypersonic laminar and forced turbulent boundary layer are visualized by the planar laser scattering technique. The effect of interaction strength on flow structures is also investigated. The results… read more here.
Keywords: incident shock; boundary layer; shock; interaction ... See more keywords
Incident shock strength evolution in overexpanded jet flow out of rocket nozzle
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DOI: 10.1016/j.actaastro.2016.11.025
Abstract: Abstract The evolution of the incident shock in the plane overexpanded jet flow or in the axisymmetric one is analyzed theoretically and compared at the whole range of governing flow parameters. Analytical results can be… read more here.
Keywords: jet; incident shock; overexpanded jet; jet flow ... See more keywords
Control of Incident Shock-Induced Separation Using Vane-Type Vortex-Generating Devices
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DOI: 10.2514/1.j056460
Abstract: An experimental investigation was conducted to control an incident shock-induced boundary-layer separation associated with a 14 deg shock generator in a Mach 2.05 flow. Two vane-type configurations... read more here.
Keywords: shock; vane type; control incident; incident shock ... See more keywords