Effects Of Shock Wave Boundary Layer Interaction On Reservoir Temperature In Shock Tunnel
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Effects Of Shock Wave Boundary Layer Interaction On Reservoir Temperature In Shock Tunnel
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Author : Munetsugu Kaneko
language : en
Publisher:
Release Date : 1999
Effects Of Shock Wave Boundary Layer Interaction On Reservoir Temperature In Shock Tunnel written by Munetsugu Kaneko and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with categories.
Data On Effects Of Incident Reflecting Shocks On The Turbulent Boundary Layer
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Author : S. Z. Pinckney
language : en
Publisher:
Release Date : 1966
Data On Effects Of Incident Reflecting Shocks On The Turbulent Boundary Layer written by S. Z. Pinckney and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamics, Hypersonic categories.
Shock Wave Boundary Layer Interactions
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Author : Holger Babinsky
language : en
Publisher: Cambridge University Press
Release Date : 2011-09-12
Shock Wave Boundary Layer Interactions written by Holger Babinsky and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2011-09-12 with Technology & Engineering categories.
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.
The Effect Of Cooling On Shock Wave Boundary Layer Interactions
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Author : Damian Anthony Sheilds
language : en
Publisher:
Release Date : 1994
The Effect Of Cooling On Shock Wave Boundary Layer Interactions written by Damian Anthony Sheilds and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with categories.
An Experimental Investigation Of Shock Wave Turbulent Boundary Layer Interactions With And Without Boundary Layer Suction
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Author : C. C. Sun
language : en
Publisher:
Release Date : 1977
An Experimental Investigation Of Shock Wave Turbulent Boundary Layer Interactions With And Without Boundary Layer Suction written by C. C. Sun and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Shock waves categories.
Tabulated data from a series of experimental studies of the interaction of a shock wave with a turbulent boundary layer in axisymmetric flow configurations is presented. The studies were conducted at the walls of circular wind tunnels and on the cylindrical centerbody of an annular flow channel. Detailed pitot pressure profiles and wall static pressure profiles upstream of, within and downstream of the interaction region are given. Results are presented for flows at nominal freestream Mach Numbers of 2, 3 and 4. For studies at the tunnel sidewalls, the shock waves were produced by conical shock generators mounted on the centerline of the wind tunnel at zero angle of attack. The annular ring generator was used to produce the shock wave at the centerbody of the annular flow channel. The effects of boundary layer bleed were examined in the investigation. Both bleed rate and bleed location were studied. Most of the bleed studies were conducted with bleed holes drilled normal to the wall surface but the effects of slot suction were also examined. A summary of the principal results and conclusions is given.
Shock Wave Interactions
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Author : Konstantinos Kontis
language : en
Publisher: Springer
Release Date : 2018-03-28
Shock Wave Interactions written by Konstantinos Kontis and has been published by Springer this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-03-28 with Technology & Engineering categories.
This edited monograph contains the proceedings of the International Shock Interaction Symposium, which emerged as an heir to both the Mach Reflection and Shock Vortex Interaction Symposia. These scientific biannual meetings provide an ideal platform to expose new developments and discuss recent challenges in the field of shock wave interaction phenomena. The goal of the symposia is to offer a forum for international interaction between young and established scientists in the field of shock and blast wave interaction phenomena. The target audience of this book comprises primarily researchers and experts in the field of shock waves, but the book may also be beneficial for young scientists and graduate students alike.
The Influence Of Shock And Boundary Layer Interaction On Shock Tube Flows
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Author : L. Davies
language : en
Publisher:
Release Date : 1967
The Influence Of Shock And Boundary Layer Interaction On Shock Tube Flows written by L. Davies and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.
During the last decade the study of the interaction between normal shocks and boundary layers in the shock tube has been carried out by many research workers. This interest has been fostered by the requirement to understand the effects that this phenomenon may have on the flow properties in the region between the reflected shock and the end of the tube. This so-called reflected shock region is important in chemical kinetics studies and as a reservoir of gas for hypersonic shock tunnels. In the paper a detailed review is given of the various analyses of the problem together with the results of experimental studies. Reflected and transmitted shock bifurcation, the rate of growth of the bifurcated foot, and the effects of transition to turbulence are discussed. The influence of bifurcation on the flow in the shock tube is assessed, especially as a mechanism for transporting cold driver gas to the end plate, causing early cooling of the gas in the reflected shock region. (Author).
Effect Of Confinement On Shock Wave Boundary Layer Interactions
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Author : Ilan Jesse Grossman
language : en
Publisher:
Release Date : 2017
Effect Of Confinement On Shock Wave Boundary Layer Interactions written by Ilan Jesse Grossman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2017 with categories.
Wall Heat Transfer Effects In The Endwall Region Behind A Reflected Shock Wave At Long Test Times
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Author : Corey Frazier
language : en
Publisher:
Release Date : 2007
Wall Heat Transfer Effects In The Endwall Region Behind A Reflected Shock Wave At Long Test Times written by Corey Frazier and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2007 with Heat categories.
Shock-tube experiments are typically performed at high temperatures ([greater than]1200K) due to test-time constraints. These test times are usually ~1 ms in duration and the source of this short, test-time constraint is loss of temperature due to heat transfer. At short test times, there is very little appreciable heat transfer between the hot gas and the cold walls of the shock tube and a high test temperature can be maintained. However, some experiments are using lower temperatures (approx. 800K) to achieve ignition and require much longer test times (up to 15 ms) to fully study the chemical kinetics and combustion chemistry of a reaction in a shock-tube experiment. Using mathematical models, analysis was performed studying the effects of temperature, pressure, shock-tube inner diameter, and test-port location at various test times (from 1-20 ms) on temperature maintenance. Three models, each more complex than the previous, were used to simulate test conditions in the endwall region behind the reflected shock wave with Ar and N2 as bath gases. Temperature profile, thermal BL thickness, and other parametric results are presented herein. It was observed that higher temperatures and lower pressures contributed to a thicker thermal boundary layer, as did shrinking inner diameter. Thus it was found that a test case such as 800K and 50 atm in a 16.2-cm-diameter shock tube in Argon maintained thermal integrity much better than other cases-- pronounced by a thermal boundary layer [less than]1 mm thick and an average temperature [greather than] 799.9 K from 1-20 ms.
Effect Of Shock Impingement On Heat Transfer
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Author : David S. Dolling
language : en
Publisher:
Release Date : 1976
Effect Of Shock Impingement On Heat Transfer written by David S. Dolling and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Heat categories.