Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degrees Sweptback Wing And A Triangular Alll Movable Control Surface
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Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degrees Sweptback Wing And A Triangular Alll Movable Control Surface
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Author : Harold L. Crane
language : en
Publisher:
Release Date : 1950
Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degrees Sweptback Wing And A Triangular Alll Movable Control Surface written by Harold L. Crane and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with 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.
Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degree Sweptback Wing And A Triangular All Movable Control Surface
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Author : Harold L. Crane
language : en
Publisher:
Release Date : 1950
Wing Flow Measurements Of Longitudinal Stability And Control Characteristics Of A Canard Airplane Configuration With A 45 Degree Sweptback Wing And A Triangular All Movable Control Surface written by Harold L. Crane and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aerofoils categories.
Measurements of the longitudinal stability and control characteristics of a canard airplane configuration have been made by the wing-flow method. The distinguishing features of this configuration in addition to the unconventional wing-stabilizer arrangement are the triangular plan form of the all-movable longitudinal control surface, the 45 degree sweptback wing of aspect ratio 4.1, and the slender body of fineness ratio 13.5. The investigation included measurements of lift, pitching moment, and rolling moment of the semispan model, with control settings between -4 degrees and 16 degrees and with the control surface removed. In some cases the angle-of-attack range was as great as from approximately -10 to 30 degrees. Approximate measurements of chord force were made at one stabilizer incidence. The Mach number range covered was from 0.55 to 1.14 at Reynolds numbers of the order of 400,000.
Subject Index To Unclassified Astia Documents
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Author : Defense Documentation Center (U.S.)
language : en
Publisher:
Release Date : 1960
Subject Index To Unclassified Astia Documents written by Defense Documentation Center (U.S.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Science categories.
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section
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Author : A. James Vitale
language : en
Publisher:
Release Date : 1954
Longitudinal Stability Characteristics At Transonic Speeds Of A Canard Configuration Having A 45 Degree Sweptback Wing Of Aspect Ratio 6 0 And Naca 65a009 Airfoil Section written by A. James Vitale and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Airplanes categories.
A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.
Longitudinal Stability And Control Characteristics At Mach Numbers Of 1 41 And 2 01 Of A 67 Degree Swept Wing Airplane Configuration With Canard Control Surfaces
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1958
Longitudinal Stability And Control Characteristics At Mach Numbers Of 1 41 And 2 01 Of A 67 Degree Swept Wing Airplane Configuration With Canard Control Surfaces 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.
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.
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.
Longitudinal Stability And Control Characteristics At Transonic Speeds Of A Semispan Airplane Model Having A 45 Degrees Sweptback Wing And Tail As Obtained By The Transonic Bump Method
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Author : M. Leroy Spearman
language : en
Publisher:
Release Date : 1948
Longitudinal Stability And Control Characteristics At Transonic Speeds Of A Semispan Airplane Model Having A 45 Degrees Sweptback Wing And Tail As Obtained By The Transonic Bump Method 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 1948 with categories.
Low Speed Static Longitudinal And Lateral Stability Characteristics Of A Variable Incidence Delta Wing Canard Model With High Lift Canard Surfaces
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Author : Clarence D. Cone (Jr.)
language : en
Publisher:
Release Date : 1959
Low Speed Static Longitudinal And Lateral Stability Characteristics Of A Variable Incidence Delta Wing Canard Model With High Lift Canard Surfaces written by Clarence D. Cone (Jr.) and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with Airplanes categories.