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Using axisymmetric analogue along the streamlines for the solution of three-dimensional viscous shock layer equations of hypersonic equilibrium flow - MaRDI portal

Using axisymmetric analogue along the streamlines for the solution of three-dimensional viscous shock layer equations of hypersonic equilibrium flow (Q3551652)

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Using axisymmetric analogue along the streamlines for the solution of three-dimensional viscous shock layer equations of hypersonic equilibrium flow
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    Using axisymmetric analogue along the streamlines for the solution of three-dimensional viscous shock layer equations of hypersonic equilibrium flow (English)
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    15 April 2010
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    viscous shock layer
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    aerodynamic heating
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    axisymmetric analogue
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    approximate method
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