The Compressible Laminar Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient PDF Download
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Author: Clarence B. Cohen Publisher: ISBN: Category : Laminar boundary layer Languages : en Pages : 43
Book Description
WIth the resulting relations, methods are derived for the calculation of the tw-dimensional and axially symmetric laminar boundary layer with an arbitrary free-stream velocity distribution, Mach number, and surface temperature.
Author: Clarence B. Cohen Publisher: ISBN: Category : Laminar boundary layer Languages : en Pages : 43
Book Description
WIth the resulting relations, methods are derived for the calculation of the tw-dimensional and axially symmetric laminar boundary layer with an arbitrary free-stream velocity distribution, Mach number, and surface temperature.
Author: Clarence B. Cohen Publisher: ISBN: Category : Aeronautics Languages : en Pages : 67
Book Description
Stewartson's transformation is applied to the laminar compressible boundary-layer equations and the requirement of similarity is introduced, resulting in a set of ordinary nonlinear differential equations previously quoted by Stewartson, but unsolved. The requirements of the system are Prandtl number of 1.0, linear viscosity-temperature relation across the boundary layer, an isothermal surface, and the particular distributions of free-stream velocity consistent with similar solutions. This system admits axial pressure gradients of arbitrary magnitude, heat flux normal to the surface, and arbitrary Mach numbers. The system of differential equations is transformed to integral system, with the velocity ratio as the independent variable. For this system, solutions are found by digital computation for pressure gradients varying from that causing separation to the infinitely favorable gradient and for wall temperatures from absolute zero to twice the free-stream stagnation temperature. Some solutions for separated flows are also presented.
Author: Clarence B. Cohen
Author: Clarence B. Cohen
Author: Harry Parrell
Author: Clarence B. Cohen![Charts and Tables for Estimating Stability of Compressible Laminar Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient [with List of References] PDF](https://books.google.com/books/content/images/frontcover/MHnqZwEACAAJ?fife=w80-h100)
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