Author: Mark J. RimlingerPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Computations of Shock-wave/boundary Layer Interactions with Bleed
Author: Mark J. RimlingerAn Investigation of Bleed Configurations and Their Effect on Shock Wave/Boundary Layer Interactions
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722228262
Category :
Languages : en
Pages : 60
Book Description
The design of high efficiency supersonic inlets is a complex task involving the optimization of a number of performance parameters such as pressure recovery, spillage, drag, and exit distortion profile, over the flight Mach number range. Computational techniques must be capable of accurately simulating the physics of shock/boundary layer interactions, secondary corner flows, flow separation, and bleed if they are to be useful in the design. In particular, bleed and flow separation, play an important role in inlet unstart, and the associated pressure oscillations. Numerical simulations were conducted to investigate some of the basic physical phenomena associated with bleed in oblique shock wave boundary layer interactions that affect the inlet performance. Hamed, Awatef Unspecified Center...
Three-dimensional Shock-wave/boundary-layer Interactions with Bleed Through Multiple Holes
Author: Mark J. RimlingerExperimental Investigation of Crossing Shock Wave-Turbulent Boundary Layer-Bleed Interaction
Author: Hyun D. KimStructure of Shock-wave/boundary Layer Interactions with Bleed Through Rows of Circular Holes
Author: T. I.-P. ShihControl of Shock Wave - Boundary Layer Interactions by Bleed in Supersonic Mixed Compression Inlets
Author: Michael K. FukudaPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 148
Book Description
Control of Shock-wave/boundary Layer Interactions with Passive Blowing and Bleeding
Author: Y.-L. LinShock 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.
Author: A. Hamed
Author: A. Hamed