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Landing Characteristics Of High Speed Wings


Landing Characteristics Of High Speed Wings
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Landing Characteristics Of High Speed Wings


Landing Characteristics Of High Speed Wings
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Author : Herbert A. Wilson
language : en
Publisher:
Release Date : 1948

Landing Characteristics Of High Speed Wings written by Herbert A. Wilson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Airplanes categories.




Approach And Landing Investigation At Lift Drag Ratios Of 2 To 4 Utilizing A Straight Wing Fighter Airplane


Approach And Landing Investigation At Lift Drag Ratios Of 2 To 4 Utilizing A Straight Wing Fighter Airplane
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Author : Gene J. Matranga
language : en
Publisher:
Release Date : 1959

Approach And Landing Investigation At Lift Drag Ratios Of 2 To 4 Utilizing A Straight Wing Fighter Airplane written by Gene J. Matranga and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Airplanes categories.




Flight Investigation Of The Low Speed Characteristics Of A 45 Deg Swept Wing Fighter Type Airplane With Blowing Boundary Layer Control Applied To The Leading And Trailing Edge Flaps


Flight Investigation Of The Low Speed Characteristics Of A 45 Deg Swept Wing Fighter Type Airplane With Blowing Boundary Layer Control Applied To The Leading And Trailing Edge Flaps
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Author :
language : en
Publisher:
Release Date : 1960

Flight Investigation Of The Low Speed Characteristics Of A 45 Deg Swept Wing Fighter Type Airplane With Blowing Boundary Layer Control Applied To The Leading And Trailing Edge Flaps 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 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 : 1955

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 1955 with Aeronautics categories.




Flight Investigation At High Speeds Of Flow Conditions Over An Airplane Wing As Indicated By Surface Tufts


Flight Investigation At High Speeds Of Flow Conditions Over An Airplane Wing As Indicated By Surface Tufts
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Author : Clotaire Wood
language : en
Publisher:
Release Date : 1945

Flight Investigation At High Speeds Of Flow Conditions Over An Airplane Wing As Indicated By Surface Tufts written by Clotaire Wood and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with Air flow categories.


Summary: Flight tests were made at high speeds with a P-47D airplane to determine the flow characteristics, as indicated by wool tufts, on a section of the upper surface of the wing. The behavior of the tufts, which were distributed over a section of the wing from 39.5 to 52.5 percent semispan, was determined from motion pictures. The tests were made in straight flight and in turns under conditions in which airplane lift coefficients from 0.10 to 0.54 and airplane Mach numbers from 0.58 to 0.78 were obtained. The results of the tests indicated that the flow remained smooth over the test panel until the critical Mach number of the panel was exceeded by 0.08 at a lift coefficient of 0.10 and by 0.05 at a lift coefficient of 0.50. Beyond these Mach numbers, the tufts indicated unsteadiness of flow and, finally, local separation when the Mach number exceeded the critical value by 0.13 at a lift coefficient of 0.10 and by 0.10 at a lift coefficient of 0.50. The region of separated flow originated in the neighborhood of 30 percent chord at high lift coefficients and 45 percent chord at low lift coefficients. Separation appeared to extend over not more than 15 percent chord.



Low Speed Investigation Of The Effects Of Large Wing Sideslip Angles On The Aerodynamic Characteristics Of Two Arrow Wing Fuselage Arrangements


Low Speed Investigation Of The Effects Of Large Wing Sideslip Angles On The Aerodynamic Characteristics Of Two Arrow Wing Fuselage Arrangements
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Author : Thomas G. Gainer
language : en
Publisher:
Release Date : 1961

Low Speed Investigation Of The Effects Of Large Wing Sideslip Angles On The Aerodynamic Characteristics Of Two Arrow Wing Fuselage Arrangements written by Thomas G. Gainer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with categories.




Annual Report Of The National Advisory Committee For Aeronautics


Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951

Annual Report Of The 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 1951 with Aeronautics 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 : 1954

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 1954 with Aeronautics categories.




Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1948

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 1948 with Mechanics, Applied categories.




The Effect Of High Wing Loading On Landing Technique And Distance With Experimental Data For The B 26 Airplane


The Effect Of High Wing Loading On Landing Technique And Distance With Experimental Data For The B 26 Airplane
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Author : F. B. Gustafson
language : en
Publisher:
Release Date : 1945

The Effect Of High Wing Loading On Landing Technique And Distance With Experimental Data For The B 26 Airplane written by F. B. Gustafson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with Aerodynamic load categories.


1. Considerations of safety and accuracy limit the rate of descent used in the landing approach to about 25 feet per second.