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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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.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22
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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 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 categories.
The static aerodynamic characteristics of a canard airplane configuration having twin vertical stabilizing surfaces are presented. The model consisted of a wing and canard both of triangular plan form and aspect ratio 2 mounted on a Sears-Haack body of fineness ratio 12.5 and two swept and tapered wing-mounted vertical tails of aspect ratio 1.35. Data are presented for Mach numbers from 0.70 to 2.22 and for angles of attack from -6 degrees to +18 degrees at 0 degrees and 5 degrees sideslip. Tests were made with the canard off and with the canard on. Nominal canard deflection angles ranged from 0 degrees to 10 degrees. The Reynolds number was 3.68 times 10 to the 6th power based on the wing mean aerodynamic chord. Selected portions of the data obtained in this investigation are compared with previously published results for the same model having a single vertical tail instead of twin vertical tails. (Author).
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 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.
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.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Triangular Wing And Canard On An Extended Body
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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 Triangular Wing And Canard On An Extended Body 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.
Low Speed Static Lateral Stability Characteristics Of A Canard Model Having A 60 Triangular Wing And Horizontal Tail
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Author : William R. Bates
language : en
Publisher:
Release Date : 1949
Low Speed Static Lateral Stability Characteristics Of A Canard Model Having A 60 Triangular Wing And Horizontal Tail written by William R. Bates and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Airplanes categories.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 7 To 2 22 Lateral Directional Characteristics Of A Triangular 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 7 To 2 22 Lateral Directional Characteristics Of A Triangular 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 categories.
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Lateral Directional Characteristics Of An Unswept Wing And Canard
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Author : Victor L. Peterson
language : en
Publisher:
Release Date : 1959
Static Stability And Control Of Canard Configurations At Mach Numbers From 0 70 To 2 22 Lateral Directional 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 1959 with categories.