Download or read book Control of Shock Wave boundary Layer Interaction by Bleed in Supersonic Mixed Compression Inlets written by Michael K. Fukuda and published by . This book was released on 1975 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Control of Shock Wave Boundary Layer Interactions by Bleed in Supersonic Mixed Compression Inlets written by Michael K. Fukuda and published by . This book was released on 1975 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Control of Shock Wave boundary Interactions by Bleed in Supersonic Mixed Compression Inlets written by Michael K. Fukuda and published by . This book was released on 1975 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock Wave Boundary Layer Interactions written by Holger Babinsky and published by Cambridge University Press. This book was released on 2011-09-12 with total page 481 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Download or read book Evaluation of Some Control volume Techniques for Analysis of Shock boundary layer Interactions in Supersonic Inlets written by Warren R. Hingst and published by . This book was released on 1975 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Two dimensional Compression Corner and Planar Shock Wave Interactions with a Supersonic Turbulent Boundary Layer written by C. Herbert Law and published by . This book was released on 1975 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Control of Shock wave boundary Layer Interactions with Passive Blowing and Bleeding written by Y.-L. Lin and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Control of the Oblique Shockwave boundary Layer Interaction in a Supersonic Inlet written by James Bellinger and published by . This book was released on 2008 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: In a supersonic engine inlet, the adverse pressure gradient caused by an oblique shockwave generated by an inlet cone interacts with low momentum boundary layer air at the inlet wall to create a region of recirculating flow called a separation bubble. This separated region reduces the effective area of the engine inlet, requiring a larger inlet to get the desired mass flow rate. As a result the engine must be larger and heavier. Over the past year, investigations have been done into the viability of controlling this oblique shockwave/boundary layer interaction with plasma actuators, using a supersonic wind tunnel simulating an engine inlet. Plasma actuators were considered for this application due to their ability to generate streamwise vortices in the flow. Vortices move low momentum boundary layer air out into the free stream and high momentum free stream air down into the boundary layer, thus increasing the momentum in the interaction region and reducing or eliminating separation. A test section containing a 10° shock generator and adjustable floor was designed and installed into an existing supersonic wind tunnel. Plasma actuators were tested at various frequencies and distances to the oblique shock impingement point, and their effect was visualized using schlieren photography.

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Computations of Shock wave boundary Layer Interactions with Bleed written by Mark J. Rimlinger and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Analysis of a Bypass Air Control System for a Supersonic Mixed compression Inlet written by Stuart C. Brown and published by . This book was released on 1967 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of Oblique Shock Boundary Layer Interaction Control written by and published by . This book was released on 1993 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this work is to provide a basic understanding of the flow in the shock boundary layer interactions and of the mechanisms of their control. A parametric investigation was conducted to determine the effect of bleed configuration on the flow in the interaction region of an incident oblique shock with a turbulent boundary layer. Results of the numerical flow simulations were obtained for different slot widths, depths and slat angles over a bleed mass flow range between zero and choked conditions. The bleed results reveal a complex structure of compression expansion wave system over the bleed port entrance, and different levels of flow operation inside the slot. Code development for the implicit numerical solution of the two dimensional compressible Navier-Stokes and K- Epsilon equations was completed. The code was used in the simulation of unsteady supersonic cavity flow and the results compared with experimental data ... Shock boundary layer bleed interactions.

Download or read book An Investigation of Shock Wave boundary Layer Interaction written by Raymond L. Chuan and published by . This book was released on 1955 with total page 114 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of the Upstream Influence of a Shock Wave at Supersonic Speeds in the Presence of a Separated Boundary Layer written by Lloyd E. Daniels and published by . This book was released on 1954 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Investigation of Shock Wave Turbulent Boundary Layer Interaction with Bleed Through Slanted Slots written by A. Hamed and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Proceedings of the 4th ASME JSME Joint Fluids Engineering Conference written by Ali Ogut and published by . This book was released on 2003 with total page 780 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Structure of Shock wave boundary Layer Interactions with Bleed Through Rows of Circular Holes written by T. I.-P. Shih and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: