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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Index To Nasa Technical Publications
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1960-07
Index To Nasa Technical Publications written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960-07 with categories.
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.
Publications Announcements
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Author : United States. National Aeronautics and Space Administration
language : en
Publisher:
Release Date : 1958
Publications Announcements written by United States. National Aeronautics and Space Administration and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aeronautics categories.
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.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1966
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aeronautics categories.
Ingenier A Aeronautica Y Astron Utica
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Author :
language : es
Publisher:
Release Date : 1963
Ingenier A Aeronautica Y Astron Utica 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.
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.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Longitudinal Characteristics Of An Unswept Wing And 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 An Unswept Wing And 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 3.1 unswept wing, an aspect ratio 3.0 unswept canard, a low aspect ratio vertical tail, and a Sears-Haack body. The hinge line of the canard was in the extended chord plane of the wing, 1.33 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.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Longitudinal Characteristics Of A Triangular Wing And Canard
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Author : John W. Boyd
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 Canard written by John W. Boyd and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with categories.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Trangular Wing And Canard With Twin Vertical Tails
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Author : Victor L. Peterson
language : en
Publisher:
Release Date : 1961
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Trangular Wing And Canard With Twin Vertical Tails 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 1961 with Aerodynamics categories.