Computation of subsonic viscous and transonic viscous-inviscid unsteady flow

A new viscous-inviscid interaction scheme is introduced, which implicitly couples the unsteady Euler and the boundary-layer equations. The adequacy of an integral formulation of the viscous flow equations for use in unsteady flows is shown in comparison with experimental results and finite-differenc...

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Veröffentlicht in:Computers & fluids 1993-07, Vol.22 (4), p.649-661
Hauptverfasser: Müller, U.R., Henke, H.
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Henke, H.
description A new viscous-inviscid interaction scheme is introduced, which implicitly couples the unsteady Euler and the boundary-layer equations. The adequacy of an integral formulation of the viscous flow equations for use in unsteady flows is shown in comparison with experimental results and finite-difference computations, and an explanation is worked out which traces back the unsteady response of the mean and turbulence field due to the external unsteadiness to a quasi-steady behaviour. The interaction computations of transonic airfoil flows by means of the Euler-boundary-layer technique are compared with the steady and unsteady experimental data sets for the RAE 2822 and the NLR 7301 supercritical airfoils, respectively.
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subjects Airfoils
Boundary layer flow
Calculations
Compressible flows
shock and detonation phenomena
Computer simulation
Exact sciences and technology
Finite difference method
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Mathematical models
Physics
Subsonic flow
Transonic flow
Viscous flow
title Computation of subsonic viscous and transonic viscous-inviscid unsteady flow
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