Numerical Solution of a Pulsating Two-dimensional Laminar Free Jet
Author : Hamid Hefazi
Publisher :
Page : 54 pages
File Size : 20,3 MB
Release : 1987
Category : Jets
ISBN :
Author : Hamid Hefazi
Publisher :
Page : 54 pages
File Size : 20,3 MB
Release : 1987
Category : Jets
ISBN :
Author : Joseph C. S. Lai
Publisher :
Page : 0 pages
File Size : 25,91 MB
Release : 1980
Category : Jets
ISBN :
The flow fields of a steady and a periodically pulsed two-dimensional turbulent free jet have been studied by solving the thin shear layer equations by the Keller Box method in transformed variable form. A constant eddy-viscosity formulation was used to model the Reynolds shear stress term. For the steady jet, calculations agree well with documented experimental data. Computed results of the unsteady jet indicate that the mean flow characteristics follow closely those of the steady jet and compare well with available experimental data. For sufficiently high frequency and amplitude of pulsation or at large streamwise distance, significant unsteady effects occur in the instantaneous quantities. (Author).
Author : S. I. Pai
Publisher :
Page : 59 pages
File Size : 43,60 MB
Release : 1969
Category :
ISBN :
Systematic numerical solutions of two dimensional and axisymmetrical laminar jet of an incompressible fluid with and without free stream were obtained. The exact numerical solutions were checked with experimental results and similarity solutions for the case without free stream. At far downstream, the numerical solutions approach the values of similarity solution. The numerical solutions give better agreement with experimental data than the similarity solutions. In general, it shows that the boundary layer equation is a good approximation of laminar jet problem provided that the Reynolds number at nozzle exit is not too low. With free stream, the numerical solutions agree with linearized analytic solution if the jet excess velocity is small in comparison with the free stream velocity. The non-linear effects are to decrease the rate of decrease of central velocity of the jet and to broaden the spread of the jet. Also an approximate numerical solution for three dimensional laminar jet is proposed. The accuracy of the method was determined from the exact solutions of the two limiting cases of three dimensional jets, i.e., two dimensional and axisymmetric. It was found that this approximate method may give good results for the axial velocity distribution and the spread of three dimensional jet. (Author).
Author : Arthur L. Mena
Publisher :
Page : 182 pages
File Size : 33,32 MB
Release : 1987
Category : Boundary layer
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Author : Arthur Louis Mena
Publisher :
Page : 182 pages
File Size : 19,31 MB
Release : 1981
Category : Boundary layer
ISBN :
Author :
Publisher :
Page : 1460 pages
File Size : 45,28 MB
Release : 1991
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author :
Publisher :
Page : 724 pages
File Size : 14,44 MB
Release : 1986
Category : Science
ISBN :
Author : United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Publisher :
Page : 1080 pages
File Size : 28,8 MB
Release : 1985
Category : Science
ISBN :
Author :
Publisher :
Page : 1090 pages
File Size : 37,25 MB
Release : 1969
Category : Mechanics, Applied
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Author :
Publisher :
Page : 1178 pages
File Size : 17,59 MB
Release : 1989
Category : Fluid dynamics
ISBN :