Numerical investigation of flow in the wake behind a finite-thickness plate upon supersonic injections from its lateral surface (Q5938980)
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scientific article; zbMATH DE number 1631364
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Numerical investigation of flow in the wake behind a finite-thickness plate upon supersonic injections from its lateral surface |
scientific article; zbMATH DE number 1631364 |
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Numerical investigation of flow in the wake behind a finite-thickness plate upon supersonic injections from its lateral surface (English)
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8 August 2001
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Boundary value problems for full Navier-Stokes equation are widely used for numerical analysis of stationary afterbody flows for plane and axisymmetric bodies. Here the authors examine the influence of a cross slit on the lateral body surface on the stationary wake flow. Numerical solutions of two-dimensional Navier-Stokes equations show a strong dependence of the flow structure on the intensity of injection and on the surface temperature of the plate.
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finite-thickness plate
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supersonic injections
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numerical simulations
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cross slit
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stationary wake flow
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two-dimensional Navier-Stokes equations
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