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Laminar and Turbulent Incompressible Boundary Layers on Slender Bodies of Revolution in Axial Flow
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The boundary-layer equations for both laminar and turbulent incompressible flows over slender bodies of revolution in axial flow are solved by an implicit finite-difference method. The Reynolds ...
Eddy-Viscosity Distribution in Thick Axisymmetric Turbulent Boundary Layers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An eddy-viscosity formulation for thick axisymmetric turbulent boundary layers is presented. Calculations made with this formulation show good agreement with experiment for both incompressible and ...
Discussion: “An Analysis of Axisymmetric Turbulent Flow Past a Long Cylinder” (White, F. M., 1972, ASME J. Basic Eng., 94, pp. 200–204)
Publisher: The American Society of Mechanical Engineers (ASME)
Skin-Friction Characteristics of Laminar Power-Law Fluids on a Slender Circular Cylinder
Publisher: The American Society of Mechanical Engineers (ASME)
A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary Layers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a finite-difference method for solving laminar and turbulent-boundary-layer equations for incompressible and compressible flows about two-dimensional and axisymmetric bodies and ...
An Inviscid-Viscous Interaction Approach to the Calculation of Dynamic Stall Initiation on Airfoils
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An interactive boundary-layer method is described for computing unsteady incompressible flows over airfoils, including the initiation of dynamic stall. The inviscid unsteady panel method developed ...
Essential Ingredients for the Computation of Steady and Unsteady Blade Boundary Layers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Two methods are described for calculating pressure distributions and boundary layers on blades subjected to low Reynolds numbers and ramp-type motion. The first is based on an interactive scheme ...
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