"Similar" Three-dimensional Boundary Layers
Author | : Theo Geis |
Publisher | : |
Total Pages | : 96 |
Release | : 1961 |
Genre | : Boundary layer |
ISBN | : |
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Author | : Theo Geis |
Publisher | : |
Total Pages | : 96 |
Release | : 1961 |
Genre | : Boundary layer |
ISBN | : |
Author | : Theo Geis |
Publisher | : |
Total Pages | : 92 |
Release | : 1961 |
Genre | : Boundary layer |
ISBN | : |
Author | : Erik Janke |
Publisher | : |
Total Pages | : 28 |
Release | : 1999 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 92 |
Release | : 1961 |
Genre | : Boundary layer |
ISBN | : |
Author | : Naval Ordnance Test Station (Inyokern, Calif.) |
Publisher | : |
Total Pages | : 42 |
Release | : 1951 |
Genre | : Boundary layer |
ISBN | : |
Author | : V. C. Patel |
Publisher | : |
Total Pages | : 32 |
Release | : 1982 |
Genre | : Turbulent boundary layer |
ISBN | : |
Three-dimensional thin boundary-layer equations for laminar and turbulent flows are solved by two different numerical schemes. The methods are applied to the flow over bodies of revolution at incidence and the results are compared with the available experimental data in order to study the range of validity of the classical boundary-layer approximations in regions of increasing circumferential gradients and flow reversal associated with the early stages of a free-vortex type of separation. Comparison with the DFVLR 6:1 spheroid data of Meier et al and the 4:1 combination-body data of Ramaprian, Patel and Choi indicate that the methods perform well in regions where the boundary layer remains thin but the predictions deteriorate as the boundary layer thickens. The results point out the need for the development of methods of handle thick boundary layers and viscous-inviscid interactions. (Author).
Author | : Hans-Hermann Fernholz |
Publisher | : Springer |
Total Pages | : 416 |
Release | : 1982 |
Genre | : Science |
ISBN | : |
Author | : James W. Christian |
Publisher | : |
Total Pages | : 103 |
Release | : 1971 |
Genre | : |
ISBN | : |
Governing equations are formulated for laminar compressible similar boundary layers with heat transfer, adverse pressure gradient, and constant cross flow. These equations are expressed in finite difference form and solved numerically. Solutions are found for attached and separated flows in adverse pressure gradients for nine combinations of cross flow and heat transfer. The purpose of these solutions is to provide understanding of how cross flow alters the two-dimensional similar results. Solutions are presented in the form of temperature profiles, main flow and cross flow velocity profiles, and global quantities; wall velocity and temperature gradients, displacement thickness, momentum thicknesses, and form factor.
Author | : |
Publisher | : |
Total Pages | : 212 |
Release | : 1972 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : |
Release | : 1984 |
Genre | : |
ISBN | : |