Longitudinal Stability And Control Characteristics At Mach Numbers From 0 70 To 2 22 Of A Triangular Wing Configuration Equipped With A Canard Control A Trailing Edge Flap Control Or A Cambered Forebody

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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.

Bulletin Signal Tique

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Author :
language : fr
Publisher:
Release Date : 1961

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 1961 with Aeronautics categories.

Longitudinal Stability And Control Characteristics At Mach Numbers From 0 70 To 2 22 Of A Triangular Wing Configuration Equipped With A Canard Control A Trailing Edge Flap Control Or A Cambered Forebody

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Author : John W. Boyd
language : en
Publisher:
Release Date : 1959

Longitudinal Stability And Control Characteristics At Mach Numbers From 0 70 To 2 22 Of A Triangular Wing Configuration Equipped With A Canard Control A Trailing Edge Flap Control Or A Cambered Forebody 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 1959 with categories.

Government Reports Annual Index

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Author :
language : en
Publisher:
Release Date : 199?

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 199? with categories.

Longitudinal Stability And Control Characteristics At Mach Numbers From 0 70 To 2 22 Of Triangular Wing Configuration Equipped With Canard Control Trailing Edge Flap Control Or Cambered Forebody With List Of References

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Author :
language : en
Publisher:
Release Date : 1959

Longitudinal Stability And Control Characteristics At Mach Numbers From 0 70 To 2 22 Of Triangular Wing Configuration Equipped With Canard Control Trailing Edge Flap Control Or Cambered Forebody With List Of References written by 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.

Longitudinal And Lateral Stability And Control Characteristics At Mach Number 2 01 Of A 60 Degree Delta Wing Airplane Configuration Equipped With A Canard Control And With Wing Trailing Edge Flap Controls

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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1958

Longitudinal And Lateral Stability And Control Characteristics At Mach Number 2 01 Of A 60 Degree Delta Wing Airplane Configuration Equipped With A Canard Control And With Wing Trailing Edge Flap Controls written by M. Leroy Spearman 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.

Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Deg Delta Wing

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Author :
language : en
Publisher:
Release Date : 1960

Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Deg Delta Wing written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 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.

Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Delta Wing

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Author : Cornelius Driver
language : en
Publisher:
Release Date : 1960

Effects Of Wing Height On The Stability And Control Characteristics At A Mach Number Of 2 01 Of A Canard Airplane Configuration With A 70 Delta Wing written by Cornelius Driver and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Airplanes 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.