Pages that link to "Item:Q1089212"
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The following pages link to Investigation of a three-dimensional hypersonic viscous shock layer on blunt bodies around which flow occurs at angles of attack and slippage (Q1089212):
Displaying 11 items.
- Three-dimensional thin viscous shock layer in the absence of planes of symmetry in the flow (Q583026) (← links)
- Numerical investigation of the hypersonic viscous shock layer on wings of infinite span at angles of attack and slip (Q800158) (← links)
- A three-dimensional hypersonic viscous shock layer in two-phase flow (Q1061588) (← links)
- Three-dimensional chemically nonequilibrium viscous shock layer on a catalytic surface with allowance for associated heat transfer (Q1081461) (← links)
- Investigation of hypersonic three-dimensional flow past blunt bodies within the framework of the parabolized Navier-Stokes equations (Q1105447) (← links)
- Investigation of the hypersonic viscous shock layer around blunt bodies in a nonuniform flow (Q1105449) (← links)
- Hypersonic three-dimensional viscous shock layer in a nonuniform gas flow in the neighborhood of the stagnation point (Q1108873) (← links)
- Flow past a three-dimensional hump in the hypersonic boundary layer on a cooled body (Q1317815) (← links)
- Three-dimensional boundary layers on complex-shaped bodies at angles of attack (Q1359926) (← links)
- Three-dimensional thermochemically nonequilibrium viscous gas flows in the neighborhood of blunt bodies (Q1402873) (← links)
- Analysis of the three-dimensional turbulent boundary layer on the surface of an arbitrary body at large angles of attack (Q1925233) (← links)
