Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6
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Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6
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Author : J. Don Gray
language : en
Publisher:
Release Date : 1972
Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6 written by J. Don Gray 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.
The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1972
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 1972 with Aeronautics categories.
A Collection Of Technical Papers
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Author :
language : en
Publisher:
Release Date : 1972
A Collection Of Technical Papers 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 Fluid dynamics categories.
Government Reports Announcements
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Author :
language : en
Publisher:
Release Date : 1972
Government Reports Announcements 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 Research categories.
Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1972
Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6 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 categories.
The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1972
Government Reports Announcements 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 1972 with Science categories.
Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1972
Effects Of Wall Cooling And Leading Edge Blunting On Ramp Induced Laminar Flow Separations At Mach Numbers From 3 Through 6 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 categories.
The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.
Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1974
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 1974 with Mechanics, Applied categories.
Government Reports Index
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Author :
language : en
Publisher:
Release Date : 1972
Government Reports 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 1972 with Government publications categories.
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1992
Nasa Sp 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 Aeronautics categories.