Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download A Theoretical Study Of Wall Cooling Effects Upon Shock Wave Laminar Boundary Layer Interaction PDF full book. Access full book title A Theoretical Study Of Wall Cooling Effects Upon Shock Wave Laminar Boundary Layer Interaction.
| Author | : Bernard G. Gautier |
| Publisher | : |
| Total Pages | : |
| Release | : 1971* |
| Genre | : Boundary layer |
| ISBN | : |
| Author | : Bernard G. Gautier |
| Publisher | : |
| Total Pages | : 100 |
| Release | : 1971 |
| Genre | : Boundary layer |
| ISBN | : |
| Author | : Holger Babinsky |
| Publisher | : Cambridge University Press |
| Total Pages | : 481 |
| Release | : 2011-09-12 |
| Genre | : Technology & Engineering |
| ISBN | : 1139498649 |
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
| Author | : David S. Dolling |
| Publisher | : |
| Total Pages | : 82 |
| Release | : 1976 |
| Genre | : |
| ISBN | : |
A theoretical parametric study has been made of adiabatic, laminar boundary layer/shock wave interactions on flat plate/convex ramp configurations. The ramp takes the form of a circular arc. This was done by using a computer program based on the integral method of Lees and Reeves recently successfully modified to include effects of streamwise ramp curvature. Primarily, the effects of different ramp radii on the overall interaction pressure distribution and other salient interaction parameters have been studied. As a further check on the theoretical model, which has already been successfully compared with experimental results at low Mach numbers, static pressure distributions throughout adiabatic laminar interactions have been measured at a free stream Mach number of 5.55. Compared to the present measured pressure distributions the theoretical model gives a satisfactory comparison downstream of the corner but overpredicts the extent of upstream influence. Furthermore, experimental pressure distributions are presented of adiabatic transitional interactions generated on convex ramp models. (Author).
| Author | : |
| Publisher | : |
| Total Pages | : 1102 |
| Release | : 1973 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : David S. Dolling |
| Publisher | : |
| Total Pages | : 34 |
| Release | : 1975 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1148 |
| Release | : 1989 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 152 |
| Release | : 1967 |
| Genre | : |
| ISBN | : |
| Author | : Michael S. Holden |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1967 |
| Genre | : Laminar boundary layer |
| ISBN | : |
| Author | : Issac Greber |
| Publisher | : |
| Total Pages | : 37 |
| Release | : 1960 |
| Genre | : Fluid mechanics |
| ISBN | : |
