Static Longitudinal Aerodynamic Characteristics Of An Elastic Canard Fuselage Configuration As Measured In Air And In Freon 12 At Mach Numbers Up To 0 92
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Static Longitudinal Aerodynamic Characteristics Of An Elastic Canard Fuselage Configuration As Measured In Air And In Freon 12 At Mach Numbers Up To 0 92
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Author : Edward Carson Yates
language : en
Publisher:
Release Date : 1963
Static Longitudinal Aerodynamic Characteristics Of An Elastic Canard Fuselage Configuration As Measured In Air And In Freon 12 At Mach Numbers Up To 0 92 written by Edward Carson Yates and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Airplanes categories.
Asme Technical Papers
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Author :
language : en
Publisher:
Release Date :
Asme 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 with Mechanical engineering categories.
Paper
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Author :
language : en
Publisher:
Release Date : 1993
Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Mechanical engineering categories.
Journal Of Aircraft
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Author :
language : en
Publisher:
Release Date : 1999
Journal Of Aircraft written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Aeronautics categories.
Bulletin Signal Tique
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Author :
language : fr
Publisher:
Release Date : 1963
Bulletin Signal Tique written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1963 with Aeronautics categories.
Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1978
Government Reports Annual 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 1978 with Government reports announcements & index categories.
Static Longitudinal Aerodynamic Characteristics Of Close Coupled Wing Canard Configurations At Mach Numbers From 1 60 To 2 86
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Author : Samuel M. Dollyhigh
language : en
Publisher:
Release Date : 1971
Static Longitudinal Aerodynamic Characteristics Of Close Coupled Wing Canard Configurations At Mach Numbers From 1 60 To 2 86 written by Samuel M. Dollyhigh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aerodynamics categories.
An experimental investigation was made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations. Three canards, ranging in exposed planform area from 17.5 to 30.0 percent of the wing reference area, were employed in this investigation. The canards were either located in the plane of the wing or in a position 18.5 percent of the wing mean geometric chord above the wing plane. Most data obtained were for a model with a 60 deg leading-edge-sweep wing; however, a small amount of data were obtained for a 44 deg leading-edge-sweep wing. The model utilized two balances to isolate interference effects between wing and canard. In general, it was determined that at angle of attack for all configurations investigated with the canard in the plane of the wing an unfavorable interference exists which causes the additional lift on the canard generated by a canard deflection to be lost on the wing due to an increased downwash at the wing from the canard. Further, this interference decreased somewhat with increasing Mach number. Raising the canard above the plane of the wing also greatly decreased the interference of the canard deflection on the wing lift. However, at Mach 2.86 the presence of the canard in the high position had a greater unfavorable interference effect at high angles of attack than the canard in the wing plane. This interference resulted in the in-plane canard having better trimmed performance at Mach 2.86 for the same center-of-gravity location.
Subsonic Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Canard Airplane Model Having A Wing With An Aspect Ratio Of 6 0
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Author :
language : en
Publisher:
Release Date : 1962
Subsonic Longitudinal Aerodynamic Characteristics Of A 1 30 Scale Canard Airplane Model Having A Wing With An Aspect Ratio Of 6 0 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 categories.
Static Longitudinal Aerodynamic Characteristics Of Close Coupled Wing Canard Configurations At Mach Numbers From 1 60 To 2 86
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Author : Samuel M. Dollyhigh
language : en
Publisher:
Release Date : 1971
Static Longitudinal Aerodynamic Characteristics Of Close Coupled Wing Canard Configurations At Mach Numbers From 1 60 To 2 86 written by Samuel M. Dollyhigh and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Aerofoils categories.
An experimental investigation has been made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coupled wing-canard configurations. Three canards, ranging in exposed planform area from 17.5 to 30.0 percent of the wing reference area, were employed in this investigation. The canards were either located in the plane of the wing or in a position 18.5 percent of the wing mean geometric chord above the wing plane. Most data obtained were for a model with a 60° leading-edge-sweep wing; however, a small amount of data were obtained for a 44° leading-edge-sweep wing. The model utilized two balances to isolate interference effects between wing and canard. In general, it was determined that at angle of attack for all configurations investigated with the canard in the plane of the wing an unfavorable interference exists which causes the additional lift on the canard generated by a canard deflection to be lost on the wing due to an increased downwash at the wing from the canard.--P. [i].
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Longitudinal Characteristics Of A Triangular Wing And Unswept Canard
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Author : Victor L. Peterson
language : en
Publisher:
Release Date : 1958
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Longitudinal Characteristics Of A Triangular Wing And Unswept Canard written by Victor L. Peterson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Airplanes categories.
The results of an investigation of the static longitudinal stability and control characteristics of a canard airplane configuration are presented without analysis for the Mach number range from 0.70 to 2.22. The configuration consisted of an aspect ratio vertical tail, and a Sears-Haack body. The hinge line of the canard was in the extended chord plane of the wing, 1.15 wing mean aerodynamic chords ahead of the reference center of moments. The ratio of the area of the exposed canard panels to the total area of the wing is 8.1 percent. Data are presented for various combinations of the canard, wing, and vertical tail for an angle-of-attack range from -6 to 18 degrees. The canard deflection angles ranged from 0 to 20 degrees.