Finite difference procedure for boundary layers including effects oflongitudinal and transverse curvatures

Y. TASSA,E. RESHOTKO, B. ANDERSON

9th Fluid and PlasmaDynamics Conference(1976)

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摘要
A second order viscous layer solution procedure has been developed that does in a consistent way include curvature effects and the corresponding normal pressure gradients. In the present system, the normal momentum equation is retained. The parabolic system of nonlinear partial differential equations is converted by linear finite differencing procedures to a system of linear algebraic equations and solved in primitive coordinates. The solutions have been shown to give smooth stable distributions for all the variables, most particularly the normal velocity which plays an important role in the interaction procedure. An algorithm for matching the viscous layer solution with a rotational characteristics outer solution has been developed.
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关键词
supersonic flow,linear algebra,curvature,flow velocity,differential equation,pressure gradient,second order,stable distribution,finite difference,pressure gradients,boundary layer,turbulent flow
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