Intersecting Shock Wave Turbulent Boundary Layer Interactions At Mach 8 3
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Intersecting Shock Wave Turbulent Boundary Layer Interactions At Mach 8 3
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-08
Intersecting Shock Wave Turbulent Boundary Layer Interactions At Mach 8 3 written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-08 with categories.
Experimental data for two three-dimensional intersecting shock-wave/turbulent boundary-layer interaction flows at Mach 8.3 are presented. The test bodies, composed of two sharp fins fastened to a flat-plate test bed, were designed to generate flows with varying degrees of pressure gradient, boundary-layer separation, and turning angle. The data include surface pressure and heat transfer distributions as well as mean flow-field surveys both in the undisturbed and interaction regimes. The data are presented in a convenient form to be used to validate existing or future computational models of these hypersonic flows. The data are also on a 3.5-inch diskette included and are available through E-mail. Kussoy, M. I. and Horstman, K. C. Ames Research Center...
Three Dimensional Shock Wave Turbulent Boundary Layer Interactions At Mach 6
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Author : C. Herbert Law
language : en
Publisher:
Release Date : 1975
Three Dimensional Shock Wave Turbulent Boundary Layer Interactions At Mach 6 written by C. Herbert Law and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamic heating categories.
Experimental results of an investigation of the three-dimensional interaction between a skewed shock wave and a turbulent boundary layer are presented. Surface pressure and heat transfer distributions and oil flow photographs were obtained at a freestream Mach number of 5.85 and two Reynolds numbers of ten and twenty million per foot. The model configuration consisted of a shock generator mounted perpendicularly to a flat plate. The shock generator leading edge was sharp and nonswept and intersected the flat plate surface about 8.5 inches downstream of the flat plate leading edge. The shock generator surface was 7.55 inches long and 3 inches high and its angle to the freestream flow was adjusted from 4 to 20 degrees. The generated shock waves were of sufficient strength to produce turbulent boundary layer separation on the flat plate surface.
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.
On 3 D Shock Wave Turbulent Boundary Layer Interactions At Mach 4
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Author : Datta Gaitonde
language : en
Publisher:
Release Date : 1996
On 3 D Shock Wave Turbulent Boundary Layer Interactions At Mach 4 written by Datta Gaitonde and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with categories.
Experiments On The Interaction With A Turbulent Boundary Layer Of A Skewed Shock Wave Of Variable Strength At Mach 2 5
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Author : L. Michael Freeman
language : en
Publisher:
Release Date : 1975
Experiments On The Interaction With A Turbulent Boundary Layer Of A Skewed Shock Wave Of Variable Strength At Mach 2 5 written by L. Michael Freeman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamic load categories.
This report covers an experimental study of the interaction of a skewed shock wave of variable strength with a turbulent boundary layer at a working Mach number of 2.5. The skewed shock wave was generated by a vertical wedge whose angle was varied in increments of 1 degree or less between 6 and 18 degrees in order to cover the spectrum of interaction from below incipient to widespread separation. Measurements include pressure distributions and oil flow photographs. The incipient separation angle was found to be between 71/2 and 8 degrees. For large wedge angles there is the appearance in the oil flow photographs of an inflection within the separated region, suggesting the possible approach to a secondary separation. The extent of separation is relatively small for angles up to 10 degrees, but grows more rapidly for larger angles. (Author).
Oblique Shock Wave Turbulent Boundary Layer Interactions In Three Dimensions At Mach 3
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Author : B. Oskam
language : en
Publisher:
Release Date : 1976
Oblique Shock Wave Turbulent Boundary Layer Interactions In Three Dimensions At Mach 3 written by B. Oskam and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.
An experimental study, thoroughly documenting the flow field and surface data resulting from the three-dimensional interaction of a shock wave, a shock generator and a high Reynolds number turbulent boundary layer, is described. Detailed surface static pressure data and heat transfer measurements are presented for 7 shock generator deflection angles ranging from 2 to 14 deg. in 2 deg. increments. The test conditions consist of a free stream Reynolds number per inch of 1.6 million, a near adiabatic wall temperature and ambient stagnation temperature. In addition to the surface data detailed flow field surveys have been conducted of time-averaged variables including flow angularity, pitot pressure, static pressure and total temperature at 2 shock generator deflection angles of 4 and 10 degrees. Detailed discussions of the experimental techniques are given which include a complete set of error estimates of the various types of data. Finally the data are presented in graphical form which may be used to analyse the problem under consideration. (Author).
Three Dimensional Shock Wave Turbulent Boundary Layer Interactions At Mach 6
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Author : C. Herbert Law
language : en
Publisher:
Release Date : 1975
Three Dimensional Shock Wave Turbulent Boundary Layer Interactions At Mach 6 written by C. Herbert Law and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with categories.
Numerical Computations Of Turbulence Amplification In Shock Wave Interactions
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Author : Thomas A. Zang
language : en
Publisher:
Release Date : 1983
Numerical Computations Of Turbulence Amplification In Shock Wave Interactions written by Thomas A. Zang and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with Shock waves categories.
Oblique Shock Wave Turbulent Boundary Layer Interactions In Three Dimensions At Mach 3
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Author : B. Oskam
language : en
Publisher:
Release Date : 1978
Oblique Shock Wave Turbulent Boundary Layer Interactions In Three Dimensions At Mach 3 written by B. Oskam and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with categories.
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.
Flow Field Measurements In A Crossing Shock Wave Turbulent Boundary Layer Interaction At Mach 3
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Author : Jason T. Lachowicz
language : en
Publisher:
Release Date : 1992
Flow Field Measurements In A Crossing Shock Wave Turbulent Boundary Layer Interaction At Mach 3 written by Jason T. Lachowicz and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.