Aerodynamic Characteristics Of A Delta Wing With Leading Edge Swept Back 45 Degrees Aspect Ratio 4 And Naca 65a006 Airfoil Section
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Aerodynamic Characteristics Of A Delta Wing With Leading Edge Swept Back 45 Degrees Aspect Ratio 4 And Naca 65a006 Airfoil Section
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Author : William C. Sleeman
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Delta Wing With Leading Edge Swept Back 45 Degrees Aspect Ratio 4 And Naca 65a006 Airfoil Section written by William C. Sleeman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerofoils categories.
This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.
Aerodynamic Characteristics Of Two Delta Wings And Two Trapezoidal Wings At Mach Number Of 4 04
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Author : Robert W. Dunning
language : en
Publisher:
Release Date : 1953
Aerodynamic Characteristics Of Two Delta Wings And Two Trapezoidal Wings At Mach Number Of 4 04 written by Robert W. Dunning and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.
Aerodynamic Characteristics Of A 45 Degree Swept Back Wing With Aspect Ratio Of 3 5 And Naca 2s 50 05 50 05 Airfoil Sections
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Author : Anthony J. Proterra
language : en
Publisher:
Release Date : 1947
Aerodynamic Characteristics Of A 45 Degree Swept Back Wing With Aspect Ratio Of 3 5 And Naca 2s 50 05 50 05 Airfoil Sections written by Anthony J. Proterra and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with categories.
Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds
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Author : John P. Mugler
language : en
Publisher:
Release Date : 1956
Effects Of Two Leading Edge Modifications On The Aerodynamic Characteristics Of A Thin Low Aspect Ratio Delta Wing At Transonic Speeds written by John P. Mugler and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Aerodynamics, Transonic categories.
An investigation was conducted in the Langley 8-foot transonic tunnel to determine the aerodynamic characteristics of a thin 60 degree delta wing with two leading-edge modifications (conical leading-edge camber and leading-edge droop) in combination with bodies with and without body indentation in accordance with the transonic-area-rule concept. The tests covered a Mach number range from 060 to 1.15 and an angle-of-attack range from -4 to 20 degrees at a Reynolds number of about 3,000,000 based on the wing mean aerodynamic chord. The wing had an aspect ratio of 2.31, a taper ratio of 0, and, without modifications, had NACA 65A003 airfoil sections parallel to the model plane of symmetry.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 60 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Airfoil Section Transonic Bump Method
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Author : Thomas J. Jr King
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 60 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Airfoil Section Transonic Bump Method written by Thomas J. Jr King and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with categories.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 35 Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
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Author : William C. Sleeman
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 35 Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section written by William C. Sleeman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aerodynamics, Transonic categories.
Research Abstracts And Reclassification Notice
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Research Abstracts And Reclassification Notice 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.
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0
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Author : Robert S. Osborne
language : en
Publisher:
Release Date : 1960
A Note On The Drag Due To Lift Of Delta Wings At Mach Numbers Up To 2 0 written by Robert S. Osborne and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Aerodynamics categories.
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.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 35 Degrees Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
DOWNLOAD
Author : William C. Sleeman
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 35 Degrees Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section written by William C. Sleeman and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with categories.