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    On the Approximate Solution of Viscous-Flow Problems 

    Source: Journal of Applied Mechanics:;1963:;volume( 030 ):;issue: 002:;page 263
    Author(s): J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The need for a general technique for the approximate solution of viscous-flow problems is discussed. Existing methods are considered and a new method is presented which results in simple ...
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    Two-Dimensional Turbulent Jet Mixing 

    Source: Journal of Applied Mechanics:;1965:;volume( 032 ):;issue: 001:;page 198
    Author(s): J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Analytic Approximations of Boundary-Layer Problems 

    Source: Journal of Applied Mechanics:;1966:;volume( 033 ):;issue: 002:;page 425
    Author(s): J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The investigation of the approximate solution of boundary-layer problems by variational techniques is extended beyond earlier work based on a single-parameter collocation approach. A multiparameter ...
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    Numerical Calculations of the Breakup of Highly Loaded Slurry Jets 

    Source: Journal of Fluids Engineering:;1987:;volume( 109 ):;issue: 003:;page 332
    Author(s): M. Situ; J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A complete numerical calculation procedure for predicting the effects of mass loading and particle diameter on laminar slurry jet breakup in a low velocity, coaxial gas stream has been developed. ...
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    Planar Free Turbulent Mixing With an Axial Pressure Gradient 

    Source: Journal of Fluids Engineering:;1967:;volume( 089 ):;issue: 004:;page 707
    Author(s): J. A. Schetz; J. Jannone
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis of incompressible free turbulent mixing processes considering either a velocity defect or excess and both favorable and adverse pressure gradients is presented. The full nonsimilar ...
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    The Rigid-Wavy-Wall Assumption in Interface Stability Problems 

    Source: Journal of Applied Mechanics:;1980:;volume( 047 ):;issue: 004:;page 949
    Author(s): P. B. Joshi; J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Transition and Mixing in the Shear Layer Produced by Tangential Injection in Supersonic Flow 

    Source: Journal of Fluids Engineering:;1971:;volume( 093 ):;issue: 004:;page 610
    Author(s): H. E. Gilreath; J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The interaction between a viscous mixing layer induced by tangential injection, and an external supersonic flow field is considered experimentally and analytically. Both subsonic and supersonic ...
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    Analysis of Multiple Jets in a Cross-Flow 

    Source: Journal of Fluids Engineering:;1982:;volume( 104 ):;issue: 004:;page 489
    Author(s): K. M. Isaac; J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Numerical Solution of the Incompressible Boundary-Layer Equations Using the Finite Element Method 

    Source: Journal of Fluids Engineering:;1992:;volume( 114 ):;issue: 004:;page 504
    Author(s): J. A. Schetz; E. Hytopoulos; M. Gunzburger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new approach to the solution of the two-dimensional, incompressible, boundary-layer equations based on the Finite Element Method in both directions is investigated. Earlier Finite Element Method ...
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    Numerical Solution of the Three-Dimensional Navier-Stokes Equations With Applications to Channel Flows and a Buoyant Jet in a Cross Flow 

    Source: Journal of Applied Mechanics:;1975:;volume( 042 ):;issue: 003:;page 575
    Author(s): J. C. Chien; J. A. Schetz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The steady, three-dimensional, incompressible Navier-Stokes equations written in terms of velocity, vorticity, and temperature are solved numerically for channel flows and a jet in a cross flow. ...
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