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Correlation Of Laminar And Transitional Heat Transfer Rates Measured In Base Type Separated Flows In A Shock Tube


Correlation Of Laminar And Transitional Heat Transfer Rates Measured In Base Type Separated Flows In A Shock Tube
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Correlation Of Laminar And Transitional Heat Transfer Rates Measured In Base Type Separated Flows In A Shock Tube


Correlation Of Laminar And Transitional Heat Transfer Rates Measured In Base Type Separated Flows In A Shock Tube
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Author : Josef Rom
language : en
Publisher:
Release Date : 1969

Correlation Of Laminar And Transitional Heat Transfer Rates Measured In Base Type Separated Flows In A Shock Tube written by Josef Rom and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1969 with categories.


Laminar heat transfer rate distributions were measured in the separated regions of a two-dimensional backward facing step, an axially symmetric backward facing step, a blunt two-dimensional base, a sharp protruding two-dimensional leading edge and in the leading edge bubble over the surface of a flat nosed two-dimensional model. The first three configurations had an initial boundary layer ahead of separation, while in the last two configurations separation occurred at the leading edge with approximately zero boundary layer thickness. All measurements were performed in the straight section of a shock tube. Maximum and average heat transfer rates were measured in the reattachment zone and over the separated region. (Author).



Scientific And Technical Aerospace Reports


Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994

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 1994 with Aeronautics categories.




Laminar And Transitional Heat Transfer In The Two Dimensional Separated Flow Behind A Sharp Protruding Leading Edge


Laminar And Transitional Heat Transfer In The Two Dimensional Separated Flow Behind A Sharp Protruding Leading Edge
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Author : Josef Rom
language : en
Publisher:
Release Date : 1967

Laminar And Transitional Heat Transfer In The Two Dimensional Separated Flow Behind A Sharp Protruding Leading Edge written by Josef Rom and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Aerothermodynamics categories.


Heat transfer rates are measured in the separated flow region behind the two-dimensional sharp protruding leading edge step model (boundary layer thickness is zero at the separation point) in the high enthalpy laminar near subsonic and supersonic flow in the shock tube. The measurements are carried out in a shock Mach number range from 2.3 to 10, and a corresponding flow Mach number range from 0.5 to 2.62. The Reynolds number, which is based on the height of the leading edge above the flat plate where the heat transfer rates are measured, varies from 300 to 17,000, and the local Reynolds number on the plate varies from 700 to 290,000. The results are correlated in terms of the non dimensional parameters of Nusselt number as a function of the Mach and Reynolds numbers and stagnation to wall enthalpy ratio. The variations of local, average and maximum heat transfer rates are presented. (Author).



Israel Journal Of Technology


Israel Journal Of Technology
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Author :
language : en
Publisher:
Release Date : 1974

Israel Journal Of Technology written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with Engineering categories.


Includes proceedings of various meetings and conferences.



Laminar Heat Transfer To A Two Dimensional Blunt Base From The High Enthalpy Flow In The Shock Tube


Laminar Heat Transfer To A Two Dimensional Blunt Base From The High Enthalpy Flow In The Shock Tube
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Author : Josef Rom
language : en
Publisher:
Release Date : 1966

Laminar Heat Transfer To A Two Dimensional Blunt Base From The High Enthalpy Flow In The Shock Tube written by Josef Rom and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.


Heat transfer rates to a two dimensional blunt base of a wedge-flat plate model are measured in a laminar supersonic flow in the shock tube. The measurements are carried out in a shock Mach number range from 2.6 to 11, and a corresponding flow Mach number range from 1.04 to 2.74. The Reynolds numbers, based on the model chord, are varied between 5000 to 500,000. The ratio of local heat transfer rate on the base to the flat plate heat transfer rate is evaluated from the measurements and the flow conditions of the various experiments. In all cases these measurements indicate a hot peak at the base center, and in some cases there are additional smaller peaks towards the base corners. The maximum and the average heat transfer rates to the base are found to be only slightly sensitive to shock Mach number, being 0.5 and 0.3 of q sub (f.p.) respectively, except in the case of choked flow (i.e. nearly sonic separation) where the average heat transfer rate approaches the value of the flat plate heat transfer rate. (Author).



U S Government Research Development Reports


U S Government Research Development Reports
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Author :
language : en
Publisher:
Release Date : 1966

U S Government Research Development 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 1966 with Science categories.




Oar Cumulative Index Of Research Results


Oar Cumulative Index Of Research Results
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Author : United States. Air Force. Office of Aerospace Research
language : en
Publisher:
Release Date : 1963

Oar Cumulative Index Of Research Results written by United States. Air Force. Office of Aerospace Research and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aeronautics categories.




Government Reports Annual Index


Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1981

Government Reports Annual 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 1981 with Government reports announcements & index categories.




A Selected Listing Of Nasa Scientific And Technical Reports For


A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1960

A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aeronautics categories.




Index Of N A S A Technical Publications


Index Of N A S A Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960

Index Of N A S A Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.