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Book An Investigation of Oblique Shock Boundary Layer Interaction Control

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.

Book Shock Wave Boundary Layer Interactions

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.

Book Investigation of an Oblique Shock Wave boundary Layer Interaction

Download or read book Investigation of an Oblique Shock Wave boundary Layer Interaction written by George Ulrich Loffert and published by . This book was released on 1964 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Investigation of the Application of Microramp Flow Control to an Oblique Shock Interaction

Download or read book Experimental Investigation of the Application of Microramp Flow Control to an Oblique Shock Interaction written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-20 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effectiveness of microramp flow control devices in controlling an oblique shock interaction was tested in the 15- by 15-Centimeter Supersonic Wind Tunnel at NASA Glenn Research Center. Fifteen microramp geometries were tested varying the height, chord length, and spacing between ramps. Measurements of the boundary layer properties downstream of the shock reflection were analyzed using design of experiments methods. Results from main effects, D-optimal, full factorial, and central composite designs were compared. The designs provided consistent results for a single variable optimization. Hirt, Stefanie M. and Anderson, Bernhard H. Glenn Research Center OBLIQUE SHOCK WAVES; BOUNDARY LAYERS; SHOCK WAVE INTERACTION; EXPERIMENT DESIGN; FACTORIAL DESIGN; SUPERSONIC WIND TUNNELS; SPACING

Book Experimental and Numerical Investigation of an Oblique Shock Wave turbulent Boundary Layer Interaction with Continuous Suction

Download or read book Experimental and Numerical Investigation of an Oblique Shock Wave turbulent Boundary Layer Interaction with Continuous Suction written by Driss Benhachmi and published by . This book was released on 1989 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Study of Mesoflaps to Control Oblique shock boundary layer Interaction

Download or read book Experimental Study of Mesoflaps to Control Oblique shock boundary layer Interaction written by Derek Lee Gefroh and published by . This book was released on 2000 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Passive Control of Oblique Shock boundary Layer Interaction at High Mach Number

Download or read book Passive Control of Oblique Shock boundary Layer Interaction at High Mach Number written by V. Borovoy and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Method for Analyzing the Interaction of an Oblique Shock Wave with a Boundary Layer

Download or read book A Method for Analyzing the Interaction of an Oblique Shock Wave with a Boundary Layer written by William C. Rose and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Method for predicting interaction produced by externally generated, oblique shock wave impinging on laminar or turbulent boundary layers.

Book Oblique Shock Wave Turbulent Boundary Layer Interactions in Three Dimensions at Mach 3

Download or read book Oblique Shock Wave Turbulent Boundary Layer Interactions in Three Dimensions at Mach 3 written by B. Oskam and published by . This book was released on 1978 with total page 181 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second phase of a detailed experimental investigation has been carried out on the interaction between oblique shock waves and turbulent boundary layers in three dimensions. The present work extends the original region of study of the shock wave interaction area towards the streamwise corner between the shock generator and the test wall. The purpose of this report is to present the experimental data in tabulated form. The tabulations include both surface data such as heat transfer and static pressure as well as detailed flow field surveys of pitot pressure, flow angularity, static pressure and total temperature.

Book Evaluation of Some Control volume Techniques for Analysis of Shock boundary layer Interactions in Supersonic Inlets

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:

Book The Interaction of an Oblique Shock Wave with a Laminar Boundary Layer

Download or read book The Interaction of an Oblique Shock Wave with a Laminar Boundary Layer written by Raimo J. Hakkinen and published by . This book was released on 1957 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Understanding Micro Ramp Control of Supersonic Shock Wave Boundary Layer Interactions

Download or read book Understanding Micro Ramp Control of Supersonic Shock Wave Boundary Layer Interactions written by and published by . This book was released on 2007 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: This research investigated the potential of micro-ramp sub-boundary layer vortex generators for flow control of oblique shock boundary layer interactions (SBLIs) which is relevant to supersonic engine inlets. These novel devices can delay shock-induced separation and improve boundary layer health, thus offering the potential to reduce the bleed requirement in intakes. Micro-ramp Experiments have been conducted at Mach 2.5, to determine the nature of flow controlled by micro-ramps and investigate their ability to delay separation in a reflected shock interaction. Various ramp sizes between 30% and 90% of boundary layer thickness were investigated. The details of the vortical flow generated by such devices was identified. The general flow features were found to scale with device height and it is suggested that smaller devices need to be placed closer to the expected adverse pressure gradients. When applied to a separated oblique shock SBLI micro-ramps were not observed to eliminate flow separation, although they were shown to break up separated regions. Other performance indicators across the SBLI were also improved through the application of the devices.

Book Experimental Investigation of the Interaction of a Plane  Oblique  Incident reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface  Volume 1   Test Description and Data Summary

Download or read book Experimental Investigation of the Interaction of a Plane Oblique Incident reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface Volume 1 Test Description and Data Summary written by and published by . This book was released on 1969 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Investigation of the Interaction of a Plane  Oblique  Incident reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface  Volume 3   Tabulated Data

Download or read book Experimental Investigation of the Interaction of a Plane Oblique Incident reflecting Shock Wave with a Turbulent Boundary Layer on a Cooled Surface Volume 3 Tabulated Data written by and published by . This book was released on 1969 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt: