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On The Compressible Laminar Boundary Layer Flow With Pressure Gradient And Heat Transfer
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Book Synopsis On the Compressible Laminar Boundary Layer Flow with Pressure Gradient and Heat Transfer by : Shoichi Uchiyama
Download or read book On the Compressible Laminar Boundary Layer Flow with Pressure Gradient and Heat Transfer written by Shoichi Uchiyama and published by . This book was released on 1957 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Pressure Gradient on the Average Convective Heat Transfer Coefficient for a Two-dimensional Laminar Compressible Boundary Layer on a Flat Plate by : Charles Pinto Howard
Download or read book The Effect of Pressure Gradient on the Average Convective Heat Transfer Coefficient for a Two-dimensional Laminar Compressible Boundary Layer on a Flat Plate written by Charles Pinto Howard and published by . This book was released on 1959 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method by : Donald Charles Baxter
Download or read book The Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method written by Donald Charles Baxter and published by . This book was released on 1957 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Calculation of Compressible Laminar Boundary Layer with Axial Pressure Gradient and Heat Transfer by : Paul A. Libby
Download or read book Method for Calculation of Compressible Laminar Boundary Layer with Axial Pressure Gradient and Heat Transfer written by Paul A. Libby and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A rapid and sufficiently accurate method, for most practical purposes, of determining laminar-boundary-layer characteristics in flow with a given free-stream Mach number and given velocity distribution at the edge of the boundary layer is presented. The method can be easily applied to flow with zero pressure gradient for any (constant) Prandtl number of the number unity and any given temperature distribution along the wall. Numerical examples are given to illustrate the method and the satisfactory accuracy obtained. For flow in an axial pressure gradient, the method can be applied for a Prandtl number of unity and any given uniform wall temperature. The methods developed here are based on an application of the Karman integral method to both the momentum and energy equations, in conjunction with a sixth-degree velocity profile and a seventh-degree stagnation-enthalpy profile. A single boundary-layer thickness and one of the coefficients in the thermal profile are the parameters in this two-parameter method.
Book Synopsis Numerical Solution of the Equations for Compressible Laminar, Transitional, and Turbulent Boundary Layers and Comparisons with Experimental Data by : Julius E. Harris
Download or read book Numerical Solution of the Equations for Compressible Laminar, Transitional, and Turbulent Boundary Layers and Comparisons with Experimental Data written by Julius E. Harris and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical method for solving the equations for laminar, transitional, and turbulent compressible boundary layers for either planar or axisymmetric flows is presented. The fully developed turbulent region is treated by replacing the Reynolds stress terms with an eddy viscosity model. The mean properties of the transitional boundary layer are calculated by multiplying the eddy viscosity by an intermittency function based on the statistical production and growth of the turbulent spots. A specifiable turbulent Prandtl number relates the turbulent flux of heat to the eddy viscosity. A three-point implicit finite-difference scheme is used to solve the system of equations. The momentum and energy equations are solved simultaneously without iteration. Numerous test cases are compared with experimental data for supersonic and hypersonic flows; these cases include flows with both favorable and mildly unfavorable pressure gradient histories, mass flux at the wall, and traverse curvature.
Book Synopsis The Compressible Laminar Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient by : Clarence B. Cohen
Download or read book The Compressible Laminar Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient written by Clarence B. Cohen and published by . This book was released on 1955 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis The Laminar Boundary Layer Equations by : N. Curle
Download or read book The Laminar Boundary Layer Equations written by N. Curle and published by Courier Dover Publications. This book was released on 2017-03-17 with total page 177 pages. Available in PDF, EPUB and Kindle. Book excerpt: Thorough introduction to boundary layer problems offers an ordered, logical presentation accessible to undergraduates. The text's careful expositions of the limitations and accuracy of various methods will also benefit professionals. 1962 edition.
Book Synopsis Laminar Flow Analysis by : David F. Rogers
Download or read book Laminar Flow Analysis written by David F. Rogers and published by Cambridge University Press. This book was released on 1992-10-30 with total page 440 pages. Available in PDF, EPUB and Kindle. Book excerpt: The major thrust of this book is to present a technique of analysis that aids the formulation, understanding, and solution of problems of viscous flow. The intent is to avoid providing a "canned" program to solve a problem, offering instead a way to recognize the underlying physical, mathematical, and modeling concepts inherent in the solutions. The reader must first choose a mathematical model and derive governing equations based on realistic assumptions, or become aware of the limitations and assumptions associated with existing models. An appropriate solution technique is then selected. The solution technique may be either analytical or numerical. Computer-aided analysis algorithms supplement the classical analyses. The book begins by deriving the Navier-Stokes equation for a viscous compressible variable property fluid. The second chapter considers exact solutions of the incompressible hydrodynamic boundary layer equations solved with and without mass transfer at the wall. Forced convection, free convection, and the compressible laminar boundary layer are discussed in the remaining chapters. The text unifies the various topics by tracing a logical progression from simple to complex governing differential equations and boundary conditions. Numerical, parametric, and directed analysis problems are included at the end of each chapter.
Book Synopsis Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method, Pt.2: Further Discussion of the Method and Computation of Examples by : Stanford University. Division of Engineering Mechanics
Download or read book Solution of Compressible Laminar Boundary Layer Problems by a Finite Difference Method, Pt.2: Further Discussion of the Method and Computation of Examples written by Stanford University. Division of Engineering Mechanics and published by . This book was released on 1957 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients by : Shimer Zane Pinckney
Download or read book Method for Predicting Compressible Turbulent Boundary Layers in Adverse Pressure Gradients written by Shimer Zane Pinckney and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (France) Publisher : ISBN 13 : Total Pages :1 pages Book Rating :4.:/5 (227 download)
Book Synopsis Effects of Heat Transfer on Laminar Boundary Layer Development Under Pressure Gradients in Compressible Flow by : ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (France)
Download or read book Effects of Heat Transfer on Laminar Boundary Layer Development Under Pressure Gradients in Compressible Flow written by ADVISORY GROUP FOR AERONAUTICAL RESEARCH AND DEVELOPMENT PARIS (France) and published by . This book was released on 1960 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Method for Calculation of Compressible Laminar Boundary Layer with Pressure Gradient and Heat Transfer by : Paul A. Libby
Download or read book Method for Calculation of Compressible Laminar Boundary Layer with Pressure Gradient and Heat Transfer written by Paul A. Libby and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Similar Solutions for the Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient by : Clarence B. Cohen
Download or read book Similar Solutions for the Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient written by Clarence B. Cohen and published by . This book was released on 1955 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
Book Synopsis The Compressible Laminar Boundary Layer with Heat Transfer and Small Pressure Gradient by : George M. Low
Download or read book The Compressible Laminar Boundary Layer with Heat Transfer and Small Pressure Gradient written by George M. Low and published by . This book was released on 1953 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The combined effects of heat transfer and pressure gradient on boundary-layer characteristics are demonstrated by applying the results of the analysis to two representative wings.
Book Synopsis Integral Methods in Compressible Laminar Boundary Layers and Their Application to Hypersonic Pressure Interactions by : Yat-Yung Chan
Download or read book Integral Methods in Compressible Laminar Boundary Layers and Their Application to Hypersonic Pressure Interactions written by Yat-Yung Chan and published by . This book was released on 1965 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Similar Solutions of the Attached and Separated Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient by : James W. Christian
Download or read book Similar Solutions of the Attached and Separated Compressible Laminar Boundary Layer with Heat Transfer and Pressure Gradient written by James W. Christian and published by . This book was released on 1970 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt: The development of governing equations and tabulation of similar solutions to the two-dimensional, laminar, compressible boundary layer with heat transfer are presented. Similar velocity and temperature profiles and global quantities such as displacement thickness, momentum thickness, form factor, etc., are presented for 116 pressure gradient-heat transfer combinations. Surface temperatures for these cases range from absolute zero (S(0) = - 1) to twice the free stream stagnation temperature (S(0) = + 1), while the streamwise pressure gradient varies from values corresponding to maximum reversed flow (beta=-0.36) to those of extremely accelerated flows (beta = 20). Results are presented at regular intervals of the parameters S(0) and beta, allowing for straight-forward comparisons between cases. Five decimal place accuracy is maintained for all results. (Author).
Book Synopsis The Theory of Laminar Boundary Layers in Compressible Fluids by : Keith Stewartson
Download or read book The Theory of Laminar Boundary Layers in Compressible Fluids written by Keith Stewartson and published by . This book was released on 1964 with total page 220 pages. Available in PDF, EPUB and Kindle. Book excerpt:
