[PDF] Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers - eBooks Review

Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers


Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers
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Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers


Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers
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Author : Albert D. Hemenover
language : en
Publisher:
Release Date : 1954

Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers written by Albert D. Hemenover and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aerofoils categories.


The effects of variation of trailing-edge angle and trailing-edge thickness on the lift characteristics of a 10-percent-chord thick symmetrical NACA airfoil section with a 25-percent-chord plain flap are appraised from wind-tunnel tests at Mach numbers from 0.3 to 0.9 and Reynolds numbers varying correspondingly from 1 to 2 million. The airfoil trailing-edge angle was varied from approximately 18 to 6 degrees, and the trailing-edge thickness from zero to the thickness at the flap hinge line.



Technical Note National Advisory Committee For Aeronautics


Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954

Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.




Research Abstracts


Research Abstracts
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date :

Research Abstracts written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Aeronautics categories.




Index Of Naca Technical Publications


Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1956

Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aeronautics categories.




Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1962

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 1962 with Mechanics, Applied 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 : 1949

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 1949 with Aeronautics categories.




Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers


Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers
DOWNLOAD
Author : Albert D. Hemenover
language : en
Publisher:
Release Date : 1951

Influence Of Airfoil Trailing Edge Angle And Trailing Edge Thickness Variation On The Effectiveness Of A Plain Flap At High Subsonic Mach Numbers written by Albert D. Hemenover and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with categories.




Current Technical Papers


Current Technical Papers
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Author :
language : en
Publisher:
Release Date : 1955

Current 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 1955 with Science categories.




Journal Of The Royal Aeronautical Society


Journal Of The Royal Aeronautical Society
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Author :
language : en
Publisher:
Release Date : 1957

Journal Of The Royal Aeronautical Society written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.




Report


Report
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Author :
language : en
Publisher:
Release Date : 1945

Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with Aeronautics categories.