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    An Approximate Method for the Solution of a Class of Nonlinear Equations in Fluid Mechanics and Magnetohydrodynamics 

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 003:;page 439
    Author(s): G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate method has been developed to obtain a closed form solution of a class of nonlinear two-point boundary value problems. Application of this method to three problems in Fluid ...
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    An Approximate Method for the Solution of a Class of Nonsimilar Laminar Boundary Layer Equations 

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 002:;page 292
    Author(s): G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An approximate method is developed for locally nonsimilar laminar boundary layer flows. This method is applicable to several boundary layer velocity problems where the nonsimilarity stems from ...
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    Initial-Value Method for a Pseudoplastic Fluid in a Laminar Boundary Layer Over a Porous Flat Plate With Suction 

    Source: Journal of Applied Mechanics:;1973:;volume( 040 ):;issue: 004:;page 1123
    Author(s): G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of finite suction velocity on the Blasius boundary-value problem, as generalized for power-law non-Newtonian fluids, has been studied by reducing the problem to an initial-value problem ...
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    Unsteady Incompressible Three-Dimensional Asymmetric Stagnation-Point Boundary Layers 

    Source: Journal of Applied Mechanics:;1980:;volume( 047 ):;issue: 002:;page 241
    Author(s): M. Kumari; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady laminar incompressible boundary-layer flow near the three-dimensional asymmetric stagnation point has been studied under the assumptions that the free-stream velocity, wall temperature, ...
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    Unsteady Incompressible Boundary-Layer Flow Over a Rotating Sphere 

    Source: Journal of Applied Mechanics:;1982:;volume( 049 ):;issue: 001:;page 234
    Author(s): M. Kumari; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
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    A Note on the Incompressible Flow Past a Semi-Infinite Flat Plate in a Stream With Uniform Shear 

    Source: Journal of Applied Mechanics:;1984:;volume( 051 ):;issue: 001:;page 210
    Author(s): J. Dey; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Compressible Boundary-Layer Swirling Flow in a Nozzle and a Diffuser With Highly Cooled Wall 

    Source: Journal of Applied Mechanics:;1979:;volume( 046 ):;issue: 002:;page 275
    Author(s): M. Kumari; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The steady laminar compressible boundary-layer swirling flow with variable gas properties and mass transfer through a conical nozzle, and a diffuser with a highly cooled wall has been studied. ...
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    Unsteady Nonsimilar Laminar Incompressible Boundary-Layer Flow Over a Yawed Infinite Circular Cylinder 

    Source: Journal of Applied Mechanics:;1985:;volume( 052 ):;issue: 002:;page 496
    Author(s): R. Vasantha; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Mass Transfer Effectiveness on Three-Dimensional Laminar Compressible Boundary Layer Flows 

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 003:;page 382
    Author(s): C. S. Vimala; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
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    An Initial Value Method for the Study of Shock-Induced Laminar Compressible Boundary Layers 

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 003:;page 367
    Author(s): C. S. Vimala; G. Nath
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An initial value method is applied for investigating laminar compressible boundary layers created by the passage of a plane shock wave over an infinite flat plate. The two point boundary value ...
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