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    Laminar and Turbulent Incompressible Boundary Layers on Slender Bodies of Revolution in Axial Flow 

    Source: Journal of Fluids Engineering:;1970:;volume( 092 ):;issue: 003:;page 545
    Author(s): T. Cebeci
    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 ...
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    Eddy-Viscosity Distribution in Thick Axisymmetric Turbulent Boundary Layers 

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 002:;page 319
    Author(s): T. Cebeci
    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 ...
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    Discussion: “An Analysis of Axisymmetric Turbulent Flow Past a Long Cylinder” (White, F. M., 1972, ASME J. Basic Eng., 94, pp. 200–204) 

    Source: Journal of Fluids Engineering:;1972:;volume( 094 ):;issue: 001:;page 204
    Author(s): T. Cebeci
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Skin-Friction Characteristics of Laminar Power-Law Fluids on a Slender Circular Cylinder 

    Source: Journal of Applied Mechanics:;1970:;volume( 037 ):;issue: 001:;page 230
    Author(s): T. Cebeci; T. Y. Na
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A Finite-Difference Method for Calculating Compressible Laminar and Turbulent Boundary Layers 

    Source: Journal of Fluids Engineering:;1970:;volume( 092 ):;issue: 003:;page 523
    Author(s): T. Cebeci; A. M. O. Smith
    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 ...
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    An Inviscid-Viscous Interaction Approach to the Calculation of Dynamic Stall Initiation on Airfoils 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 004:;page 714
    Author(s): T. Cebeci; M. F. Platzer; H. M. Jang; H. H. Chen
    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 ...
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    Essential Ingredients for the Computation of Steady and Unsteady Blade Boundary Layers 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 608
    Author(s): H. M. Jang; J. A. Ekaterinaris; M. F. Platzer; T. Cebeci
    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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