Theoretical Characteristics in Supersonic Flow of Constant-Chord Partial-Span Control Surfaces on Rectangular Wings PDF Download
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Languages : en
Pages : 0
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Languages : en
Pages : 0
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Author: Warren A. Tucker
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 19
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Equations were found for the lift coefficient, rolling-moment coefficient, and hinge-moment coefficient due to control deflection, and for the pitching-moment coefficient due to flap lift. The effect of thickness was shown to be given by a single factor.
Author: Warren A. Tucker
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 25
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A theoretical analysis was made of the characteristics of constant-chord, full-span control surfaces on thin triangular wings at supersonic speeds by use of methods based on the linearized equation for supersonic flow. Expressions were found for lift effectiveness, pitching-moment coefficient, hinge-moment coefficient due to control deflection, and hinge-moment coefficient due to angle of attack. These expressions were given as functions of the ratio of flap chord to wing chord and the ratio of the tangent of the wing-semiapex angle to the tangent of the Mach angle.
Author: Robert O. Piland
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Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
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The theoretical lift and pitching moment due to angle of attack and pitching and the lateral force and yawing moment due to rolling of a trapezoidal wing are derived. The equations are applicable when the inboard Mach line from a leading-edge tip intersects the trailing edge and the outboard Mach line lies ahead of the side edge. When the side edges are raked in, the former condition is sufficient. A comparison based on theoretical expressions of the lift and rolling effectiveness for half-delta tip (point forward) and trailing-edge flaps on various plan forms is made.
Author: United States. National Advisory Committee for Aeronautics
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Category : Aeronautics
Languages : en
Pages : 1056
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 692
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Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Author:
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Category : Aeronautics
Languages : en
Pages : 620
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Category :
Languages : en
Pages : 424
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Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 162
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Author:
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Category : Mechanics, Applied
Languages : en
Pages : 1096
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