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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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.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 45 Degrees Aspect Ratio 4 Taper Ratio 0 3 And Naca 65a006 Airfoil Section
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Author : Boyd C. Myers
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 45 Degrees Aspect Ratio 4 Taper Ratio 0 3 And Naca 65a006 Airfoil Section written by Boyd C. Myers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Airplane categories.
This paper presents the results of the investigation of a wing-alone and wing-fuselage configuration employing a wing with the quarter-chord line swept back 45 degrees, with aspect ratio 4, taper ratio 0.3, 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 were also obtained for these configurations and are presented for a range of tail heights at one tail length. In order to expedite the publishing of these data, only a brief analysis is included.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 60 Degrees Aspect Ratio 2 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
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Author : Boyd C. Myers
language : en
Publisher:
Release Date : 1950
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 60 Degrees Aspect Ratio 2 Taper Ratio 0 6 And Naca 65a006 Airfoil Section written by Boyd C. Myers and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Airplanes categories.
This paper presents the results of the investigation of a wing-alone and a wing-fuselage configuration employing a wing with quarter-chord line swept back 60 degrees, aspect ratio 2, taper ratio 0.6, and an NACA 65A006 airfoil section. The results are presented as lift, drag, pitching-moment and bending-moment coefficients for both configurations. In addition, effective downwash angles and point dynamic pressures for a range of tail heights at a probable tail length are presented for the two configurations investigated.
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 A Wing With Quarter Chord Line Swept Back 35 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Aifoil Section Transonic Bump Method
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Author : William C. Jr Sleeman
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 35 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Aifoil Section Transonic Bump Method written by William C. Jr 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.
Aerodynamic Characteristics Of A Wing With Quarter Chord Swept Back 60 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
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Author : Thomas J. King
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Swept Back 60 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Airfoil Section written by Thomas J. 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 Aerofoils categories.
This paper presents the results of the investigation of a wing-alone and a wing-fuselage configuration employing a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section. The results are presented as lift, drag, pitching-moment, and bending moment coefficients for both configurations. The effect of a wing fence on the wing-fuselage characteristics was also investigated. In addition, effective downwash angles and point dynamic pressures for a range of tail heights at a probable tail length are presented for the two configurations investigated. Only a brief analysis is given in order to facilitate the publishing of the data.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 45 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
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Author : Joseph Weil
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 45 Degrees Aspect Ratio 4 Taper Ratio 0 6 And Naca 65a006 Airfoil Section written by Joseph Weil 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.
As part of an NACA research program, a series of wing-body combinations are being investigated in the Langley high-speed 7- by 10-foot tunnel up to a Mach number of 1.18 utilizing the transonic bump.
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 45 Degrees Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section
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Author : Kenneth W. Goodson
language : en
Publisher:
Release Date : 1949
Aerodynamic Characteristics Of A Wing With Quarter Chord Line Swept Back 45 Degrees Aspect Ratio 6 Taper Ratio 0 6 And Naca 65a006 Airfoil Section written by Kenneth W. Goodson 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 a wing-alone and a wing-fuselage configuration employing a wing with the quarter-chord line swept back 45 degrees, aspect ratio 6, taper ratio 0.6, 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 configurations and are presented for a range of tail heights at one tail length. In order to expedite the publishing of these data, only a brief analysis is included.
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
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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 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.