ENGLISH

Shock Wave-Boundary-Layer Interactions

By Holger Babinsky , John K. Harvey

Book information

Publisher
Cambridge University Press
Year
2011
ISBN
0521848520, 9780521848527
LCC
TL574.S4 S575 2011
Google Books ID
3nIU5zS-94YC
Open Library ID
OL25108780M
Language
english
Format
PDF
Filesize
12 MB (12584504 bytes)
Series
Cambridge Aerospace
Pages
480\480
Orientation
yes
Scanned
no
Time added
2012-03-09 12:00:00
Механика;Механика жидкостей и газов;Гидрогазодинам

Description

Shock Wave/Boundary Layer Interaction (SBLI) is a fundamental phenomenon in gasdynamics and frequently a defining feature in high speed aerodynamic flowfields. The interactions can be found in practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLI's have the potential to pose serious problems and is thus a critical issue for aerospace applications. This is the first book devoted solely to a comprehensive, state of the art explanation of the phenomenon with coverage of all flow regimes where SBLI's occur. The book includes contributions from leading international experts who share their insight into SBLI physics and the impact of these interactions on practical flow situations. This book is aimed at practitioners and graduate students in aerodynamics who wish to familiarise themselves with all aspects of SBLI flows. It is a valuable resource for the specialist because it gathers experimental, computational and theoretical knowledge in one place.

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