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| Author | : K. D. P. Sinha |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1954 |
| Genre | : |
| ISBN | : |
| Author | : Aeronautical Research Council |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1956 |
| Genre | : Laminar boundary layer |
| ISBN | : |
| Author | : Aeronautical Research Council |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1956 |
| Genre | : Laminar boundary layer |
| ISBN | : |
| Author | : Lewis Frederick Crabtree |
| Publisher | : |
| Total Pages | : 202 |
| Release | : 1952 |
| Genre | : Air flow |
| ISBN | : |
| Author | : Aeronautical Research Council |
| Publisher | : |
| Total Pages | : 37 |
| Release | : 1956 |
| Genre | : Laminar flow |
| ISBN | : |
| Author | : G. V. Lachmann |
| Publisher | : Elsevier |
| Total Pages | : 768 |
| Release | : 2014-05-12 |
| Genre | : Technology & Engineering |
| ISBN | : 1483226662 |
Boundary Layer and Flow Control: Its Principles and Application, Volume 2 focuses on the layer of fluid in the immediate area of a bounding surface where the effects of viscosity are substantial. This book is organized into two main topics—boundary layer control for low drag, and shock-induced separation and its prevention by design and boundary layer control. It specifically discusses the nature of transition, effect of two-dimensional and isolated roughness on laminar flow, and progress in the design of low drag aerofoils. The onset of separation effects for aerofoils and wings, shock-induced separation for laminar boundary layers, and shock-induced separation for laminar boundary layers are also deliberated. This volume is recommended to physicists and specialists interested in boundary layer and flow control.
| Author | : |
| Publisher | : |
| Total Pages | : 62 |
| Release | : 1950 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Eli Reshotko |
| Publisher | : |
| Total Pages | : 86 |
| Release | : 1957 |
| Genre | : Aerodynamic heating |
| ISBN | : |
The equations for development of the compressible laminar boundary layer over a yawed infinite cylinder are presented. For compressible flow with a pressure gradient the chordwise and spanwise flows are not independent. By use of the Stewartson transformation and a linear viscosity-temperature relation, a set of three simultaneous ordinary differential equations is obtained in a form yielding similar solutions. These equations are solved for stagnation-line flow for surface temperatures from zero to twice the free-stream stagnation temperature and for a wide range of yaw angle and free-stream Mach number.
| Author | : Leonid Filippovich Kozlov |
| Publisher | : |
| Total Pages | : 186 |
| Release | : 1970 |
| Genre | : Boundary layer |
| ISBN | : |
| Author | : A. W. Lindfield |
| Publisher | : |
| Total Pages | : |
| Release | : 1957 |
| Genre | : |
| ISBN | : |
