Theoretical Investigation of 3-D Shock Wave-turbulent Boundary Layer Interactions
Author | : Doyle D. Knight |
Publisher | : |
Total Pages | : 80 |
Release | : 1988 |
Genre | : Navier-Stokes equations |
ISBN | : |
Download A Numerical Investigation Of 3 D Shock Wave Turbulent Boundary Layer Interactions Generated By The Sharp Fin And Swept Compression Corner full books in PDF, epub, and Kindle. Read online free A Numerical Investigation Of 3 D Shock Wave Turbulent Boundary Layer Interactions Generated By The Sharp Fin And Swept Compression Corner ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Doyle D. Knight |
Publisher | : |
Total Pages | : 80 |
Release | : 1988 |
Genre | : Navier-Stokes equations |
ISBN | : |
Author | : J. Delery |
Publisher | : Springer Science & Business Media |
Total Pages | : 434 |
Release | : 2013-03-08 |
Genre | : Science |
ISBN | : 3642827705 |
It was on a proposal of the late Professor Maurice Roy, member of the French Academy of Sciences, that in 1982, the General Assembly of the International Union of Theoretical and Applied Mechanics decided to sponsor a symposium on Turbulent Shear-Layer/Shock-Wave Interactions. This sympo sium might be arranged in Paris -or in its immediate vicinity-during the year 1985. Upon request of Professor Robert Legendre, member of the French Academy of Sciences, the organization of the symposium might be provided by the Office National d'Etudes et de Recherches Aerospatiales (ONERA). The request was very favorably received by Monsieur l'Ingenieur General Andre Auriol, then General Director of ONERA. The subject of interactions between shock-waves and turbulent dissipative layers is of considerable importance for many practical devices and has a wide range of engineering applications. Such phenomena occur almost inevitably in any transonic or supersonic flow and the subject has given rise to an important research effort since the advent of high speed fluid mechanics, more than forty years ago. However, with the coming of age of modern computers and the development of new sophisticated measurement techniques, considerable progress has been made in the field over the past fifteen years. The aim of the symposium was to provide an updated status of the research effort devoted to shear layer/shock-wave interactions and to present the most significant results obtained recently.
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.