Author: Bernard G. GautierPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100
Book Description
A Theoretical Study of Wall Cooling Effects Upon Shock Wave-laminar Boundary Layer Interaction by the Method of Lees-reeves-klineberg
Author: Bernard G. GautierPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger BabinskyPublisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
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.
Scientific and Technical Aerospace Reports
Author: Applied Mechanics Reviews
Author: Air Force Research Resumés
Author: A Review of High-speed, Convective, Heat-transfer Computation Methods
Author: Michael E. TauberPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
The Aeronautical Journal
Author: 29th International Symposium on Shock Waves 2
Author: Riccardo BonazzaPublisher: Springer
ISBN: 331916838X
Category : Science
Languages : en
Pages : 822
Book Description
This proceedings present the results of the 29th International Symposium on Shock Waves (ISSW29) which was held in Madison, Wisconsin, U.S.A., from July 14 to July 19, 2013. It was organized by the Wisconsin Shock Tube Laboratory, which is part of the College of Engineering of the University of Wisconsin-Madison. The ISSW29 focused on the following areas: Blast Waves, Chemically Reactive Flows, Detonation and Combustion, Facilities, Flow Visualization, Hypersonic Flow, Ignition, Impact and Compaction, Industrial Applications, Magnetohydrodynamics, Medical and Biological Applications, Nozzle Flow, Numerical Methods, Plasmas, Propulsion, Richtmyer-Meshkov Instability, Shock-Boundary Layer Interaction, Shock Propagation and Reflection, Shock Vortex Interaction, Shock Waves in Condensed Matter, Shock Waves in Multiphase Flow, as well as Shock Waves in Rarefield Flow. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 29 and individuals interested in these fields.
Aeronautical Engineering Review
Author: Improved Computer Program for Calculation of Viscous-inviscid Interactions
Author: Bernard G. GautierPublisher:
ISBN:
Category : Viscous flow
Languages : en
Pages : 250
Book Description
The report describes a theoretical and experimental investigation of the effect of wall cooling on the overall features of shock wave laminar boundary layer interactions in hypersonic two dimensional flow. The integral method of Lees-Reeves-Klineberg has been modified in order to compute viscous interactions over a continuous range of wall-to-stagnation temperature ratios using a single set of 'universal' integral functions. Comparisons between the theoretical predictions and the experimental results obtained from pressure and heat transfer distribution measurements show satisfactory agreements. (Modified author abstract).