Theoretical Characteristics in Supersonic Flow of Constant-chord Partial-span Control Surfaces on Rectangular Wings Having Finite Thickness PDF Download
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Author: Warren A. Tucker
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 19
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Book Description
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
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 19
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Book Description
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:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Author: Robert O. Piland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
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Book Description
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
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1056
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 692
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Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Author: Bruce T. Lundin
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 262
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 424
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Author: Max A. Heaslet
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 656
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Book Description
Under the assumptions of linearized theory, general methods of solutin are given for two- and three-dimensional steady-state and two-dimensional unsteady-state equations of compressible flow. The solutions depend in all cases on the use of Green's equivalent layer of sources, sinks, and doublets. Emphasis is placed on applications in supersonic wing theory, the singularities arising in the integrations being treated by Hadamard's finite part of the technique. Four examples of different character are discussed. In particular, the load distribution over a specific swept-back lifting surface is determined at a free-stream Mach number of one.
Author: Arthur L. Jones
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 644
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Book Description
The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.
