The Effect Of Impinging Periodic Shock Waves On Heat Transfer To A Cooled Wall
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The Effect Of Impinging Periodic Shock Waves On Heat Transfer To A Cooled Wall
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Author : Harold George Weber
language : en
Publisher:
Release Date : 1973
The Effect Of Impinging Periodic Shock Waves On Heat Transfer To A Cooled Wall written by Harold George Weber and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1973 with categories.
Comprehensive Dissertation Index
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Author :
language : en
Publisher:
Release Date : 1989
Comprehensive Dissertation Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Dissertations, Academic categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1993
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.
Annual Report Engineering Experiment Station University Of Wisconsin Madison
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Author : University of Wisconsin--Madison. Engineering Experiment Station
language : en
Publisher:
Release Date : 1972
Annual Report Engineering Experiment Station University Of Wisconsin Madison written by University of Wisconsin--Madison. Engineering Experiment Station and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Engineering categories.
Annual Report Engineering Experiment Station University Of Wisconsin
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Author : University of Wisconsin. Engineering Experiment Station
language : en
Publisher:
Release Date : 1972
Annual Report Engineering Experiment Station University Of Wisconsin written by University of Wisconsin. Engineering Experiment Station and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with categories.
Effects Of Shock Wave Impingement On The Heat Transfer On A Cylindrical Leading Edge
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Author : Robert S. Hiers
language : en
Publisher:
Release Date : 1967
Effects Of Shock Wave Impingement On The Heat Transfer On A Cylindrical Leading Edge written by Robert S. Hiers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Heat categories.
The Effect Of Periodic Shock Fronted Pressure Waves On The Instantaneous Heat Flux At The End Wall Of A Tube
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Author : Raymond William Goluba
language : en
Publisher:
Release Date : 1968
The Effect Of Periodic Shock Fronted Pressure Waves On The Instantaneous Heat Flux At The End Wall Of A Tube written by Raymond William Goluba and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with Heat categories.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1972
Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Mechanics, Applied categories.
American Doctoral Dissertations
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Author :
language : en
Publisher:
Release Date : 1992
American Doctoral Dissertations written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with Dissertation abstracts categories.
Experimental Studies Of Shock Wave Wall Jet Interaction In Hypersonic Flow
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-24
Experimental Studies Of Shock Wave Wall Jet Interaction In Hypersonic Flow 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 2018-07-24 with categories.
Experimental studies have been conducted to examine slot film cooling effectiveness and the interaction between the cooling film and an incident planar shock wave in turbulent hypersonic flow. The experimental studies were conducted in the 48-inch shock tunnel at Calspan at a freestream Mach number of close to 6.4 and at a Reynolds number of 35 x 10(exp 6) based on the length of the model at the injection point. The Mach 2.3 planar wall jet was generated from 40 transverse nozzles (with heights of both 0.080 inch and 0.120 inch), producing a film that extended the full width of the model. The nozzles were operated at pressures and velocities close to matching the freestream, as well as at conditions where the nozzle flows were over- and under-expanded. A two-dimensional shock generator was used to generate oblique shocks that deflected the flow through total turnings of 11, 16, and 21 degrees; the flows impinged downstream of the nozzle exits. Detailed measurements of heat transfer and pressure were made both ahead and downstream of the injection station, with the greatest concentration of measurements in the regions of shock-wave/boundary layer interaction. The major objectives of these experimental studies were to explore the effectiveness of film cooling in the presence of regions of shock-wave/boundary layer interaction and, more specifically, to determine how boundary layer separation and the large recompression heating rates were modified by film cooling. Detailed distributions of heat transfer and pressure were obtained in the incident-shock/wall-jet interaction region for a series of shock strengths and impingement positions for each of the two nozzle heights. Measurements were also made to examine the effects of nozzle lip thickness on cooling effectiveness. The major conclusion from these studies was that the effect of the cooling film could be readily dispersed by relatively weak incident shocks, so the peak heating in the recompression region was not sig...