Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF Download

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Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail

Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF Author: William R. Bates
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail

Low-speed Static Longitudinal Stability Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF Author: William R. Bates
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail

Low-speed Static Lateral Stability Characteristics of a Canard Model Having a 60© Triangular Wing and Horizontal Tail PDF Author: William R. Bates
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38

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Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface

Low-speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface PDF Author: John W. Draper
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 43

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Book Description
An investigation has been made of the low-speed static stability characteristics of a canard model with a 45 degree sweptback wing and a 60 degree triangular horizontal control surface. The model had practically no allowable center-of-gravity range because of longitudinal instability that occurred at moderate and high lift coefficients with horizontal-control-surface incidences of 10 degrees or less. The horizontal control surface produced a sidewash which, at an incidence of 15 degrees at angles of attack greater than 7 degrees, was strong enough to make the model directionally stable with the vertical tail off. This sidewash caused a vertical tail mounted on the fuselage to be destabilizing at angles of attack above 11 degrees. Twin vertical tails mounted at the wing tips did not produce a similar destabilizing effect because they were located outside the sidewash field.

Low-speed Static Lateral-stabilty Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail

Low-speed Static Lateral-stabilty Characteristics of a Canard Model Having a 60 Degree Triangular Wing and Horizontal Tail PDF Author: William R. Bates
Publisher:
ISBN:
Category :
Languages : en
Pages : 29

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Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces

Low-speed Static Longitudinal and Lateral Stability Characteristics of a Variable-incidence Delta-wing Canard Model with High-lift Canard Surfaces PDF Author: Clarence D. Cone (Jr.)
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 76

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The Low-speed Static Longitudinal and Lateral Characteristics of a Delta-wing Model with Fixed and Free-floating Canard Surfaces

The Low-speed Static Longitudinal and Lateral Characteristics of a Delta-wing Model with Fixed and Free-floating Canard Surfaces PDF Author: William I. Scallion
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 64

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails

Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category :
Languages : en
Pages : 45

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Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails

Effects of Horizontal-tail Position, Area, and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degrees Triangular-wing Model Having Various Triangular-all-movable Horizontal Tails PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category :
Languages : en
Pages : 61

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580

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Book Description