An Approximate Method of Calculating the Laminar Boundary Layer in Two-dimensional Incompressible Flow
Author : M.R. Head
Publisher :
Page : pages
File Size : 48,24 MB
Release : 1957
Category :
ISBN :
Author : M.R. Head
Publisher :
Page : pages
File Size : 48,24 MB
Release : 1957
Category :
ISBN :
Author : Aeronautical Research Council
Publisher :
Page : 53 pages
File Size : 13,32 MB
Release : 1959
Category : Laminar boundary layer
ISBN :
Author : M. R. Head
Publisher :
Page : 53 pages
File Size : 14,45 MB
Release : 1959
Category :
ISBN :
Author : Lev Gerasimovich Loĭt︠s︡i︠a︡nskiĭ
Publisher :
Page : 28 pages
File Size : 24,55 MB
Release : 1951
Category : Aerodynamics
ISBN :
A method is given for the approximate solution of the equations of the two-dimensional laminar boundary layer in an incompressible fluid. The method is based on the use of a system of equations of successive moments that is easily solved for simple supplementary assumptions. The solution obtained is given in closed form by simple formulas and is claimed to be no less accurate than the complicated solutions previously obtained, which were based on the use of special classes of flows.
Author : Coleman duP. Donaldson
Publisher :
Page : 26 pages
File Size : 12,72 MB
Release : 1949
Category : Aerodynamics
ISBN :
Abstract: An approximate method is presented for the estimation of the properties of the incompressible laminar boundary layer on a flat plate in the slip-flow regime using Kármán's momentum method. These results are compared with results for a normal boundary layer at the same Reynolds number to bring out the characteristics of a slip boundary layer. A simple criterion for the importance of slip is presented.
Author : Erich Truckenbrodt
Publisher :
Page : 48 pages
File Size : 18,59 MB
Release : 1955
Category : Aerodynamics
ISBN :
Abstract: For calculation of the characteristic parameters of the boundary layer (momentum-loss thickness and form parameter for the velocity profile), two quadrature formulas are given which are valid for the laminar as well as for the turbulent state of flow. These formulas cover both the two-dimensional and the rotationally symmetrical case. The calculation of the momentum-loss thickness is carried out by a simple integration of the energy theorem. The equation for the form parameter is obtained by coupling of the momentum theorem with the energy theorem. Knowledge of the derivatives of the velocity distribution and of the radius of the body along the length x is not necessary.
Author : Leonid Aleksandrovich Rozin
Publisher :
Page : 16 pages
File Size : 22,41 MB
Release : 1960
Category : Boundary layer
ISBN :
Author : Nicholas Drennan Brown
Publisher :
Page : 60 pages
File Size : 50,28 MB
Release : 1969
Category :
ISBN :
Author : E.C. Maskell
Publisher :
Page : 50 pages
File Size : 29,91 MB
Release : 1951
Category :
ISBN :
Author : Tuncer Cebeci
Publisher :
Page : 42 pages
File Size : 37,70 MB
Release : 1977
Category : Laminar flow
ISBN :