Stagger Angle Effects On Impingement Cooling Of A Rotating Turbine Blade
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Stagger Angle Effects On Impingement Cooling Of A Rotating Turbine Blade
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Author : Uriel Z. Preiser
language : en
Publisher:
Release Date : 1983
Stagger Angle Effects On Impingement Cooling Of A Rotating Turbine Blade written by Uriel Z. Preiser and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.
Channel Flow Modeling Of Impingement Cooling Of A Rotating Turbine Blade
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Author : JaHye Jenny Koo
language : en
Publisher:
Release Date : 1984
Channel Flow Modeling Of Impingement Cooling Of A Rotating Turbine Blade written by JaHye Jenny Koo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with categories.
Effects Of Rotation On Impingement Cooling Of Turbine Blades With Chordwise Exhaust At Zero Stagger Angle
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Author : Earl William Renaud
language : en
Publisher:
Release Date : 1987
Effects Of Rotation On Impingement Cooling Of Turbine Blades With Chordwise Exhaust At Zero Stagger Angle written by Earl William Renaud and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with categories.
Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades
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Author : J.C. Kreatsoulas
language : en
Publisher:
Release Date : 1987
Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades written by J.C. Kreatsoulas and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with categories.
Experimental Study Of Impingement Cooling In Rotating Turbine Blades
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Author : Massachusetts Institute of Technology. Gas Turbine & Plasma Dynamics Laboratory
language : en
Publisher:
Release Date : 1983
Experimental Study Of Impingement Cooling In Rotating Turbine Blades written by Massachusetts Institute of Technology. Gas Turbine & Plasma Dynamics Laboratory and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.
Jet Impingement Cooling In Rotating Coolant Passages Of Gas Turbine Blades
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Author : Kumar Vyaghreswara Akella
language : en
Publisher:
Release Date : 1998
Jet Impingement Cooling In Rotating Coolant Passages Of Gas Turbine Blades written by Kumar Vyaghreswara Akella and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
The Effects Of Surface Roughness Of Impingement Cooling Of A Gas Turbine Blade
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Author : Eric R. McFarland
language : en
Publisher:
Release Date : 1974
The Effects Of Surface Roughness Of Impingement Cooling Of A Gas Turbine Blade written by Eric R. McFarland and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1974 with categories.
The Effects Of Rotation On Heat Transfer In Turbine Blade Cooling
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Author : Andrew Jones
language : en
Publisher:
Release Date : 1994
The Effects Of Rotation On Heat Transfer In Turbine Blade Cooling written by Andrew Jones 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.
Effect Of Rotation On Flow In A Ribbed Rotating Turbine Blade Cooling Duct Model
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Author : Rahul Bharadwaj
language : en
Publisher:
Release Date : 2002
Effect Of Rotation On Flow In A Ribbed Rotating Turbine Blade Cooling Duct Model written by Rahul Bharadwaj and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with categories.
Experimental Investigation Of Turbine Blade Platform Film Cooling And Rotational Effect On Trailing Edge Internal Cooling
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Author : Lesley Mae Wright
language : en
Publisher:
Release Date : 2010
Experimental Investigation Of Turbine Blade Platform Film Cooling And Rotational Effect On Trailing Edge Internal Cooling written by Lesley Mae Wright and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2010 with categories.
The present work has been an experimental investigation to evaluate the applicability of gas turbine cooling technology. With the temperature of the mainstream gas entering the turbine elevated above the melting temperature of the metal components, these components must be cooled, so they can withstand prolonged exposure to the mainstream gas. Both external and internal cooling techniques have been studied as a means to increase the life of turbine components. Detailed film cooling effectiveness distributions have been obtained on the turbine blade platform with a variety of cooling configurations. Because the newly developed pressure sensitive paint (PSP) technique has proven to be the most suitable technique for measuring the film effectiveness, it was applied to a variety of platform seal configurations and discrete film flows. From the measurements it was shown advanced seals provide more uniform protection through the passage with less potential for ingestion of the hot mainstream gases into the engine cavity. In addition to protecting the outer surface of the turbine components, via film cooling, heat can also be removed from the components internally. Because the turbine blades are rotating within the engine, it is important to consider the effect of rotation on the heat transfer enhancement within the airfoil cooling channels. Through this experimental investigation, the heat transfer enhancement has been measured in narrow, rectangular channels with various turbulators. The present experimental investigation has shown the turbulators, coupled with the rotation induced Coriolis and buoyancy forces, result in non-uniform levels of heat transfer enhancement in the cooling channels. Advanced turbulator configurations can be used to provide increased heat transfer enhancement. Although these designs result in increased frictional losses, the benefit of the heat transfer enhancement outweighs the frictional losses.