Approximate Relations for Hinge-moment Parameters of Control Surfaces on Swept Wings at Low Mach Numbers

Approximate Relations for Hinge-moment Parameters of Control Surfaces on Swept Wings at Low Mach Numbers
Author: Thomas A. Toll
Publisher:
Total Pages: 17
Release: 1948
Genre: Airplanes
ISBN:

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This report contains derivations, based on an approximate theory, of equations for the hinge-moment parameters of control surfaces on swept wings at low Mach numbers. Method accounts for effects of sweep and aspect ratio, and considers, in an approximate manner, the effects of induced camber. Comparisons of calculated and experimental values of the hinge-moment parameters are presented.

The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow

The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Author: Arthur L. Jones
Publisher:
Total Pages: 644
Release: 1948
Genre: Aerodynamics, Supersonic
ISBN:

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The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.

Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration

Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration
Author: Frank S. Malvestuto
Publisher:
Total Pages: 842
Release: 1951
Genre: Aerodynamics, Supersonic
ISBN:

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Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.

Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 1370
Release: 1949
Genre: Aeronautics
ISBN:

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Method for Calculating Lift Distribtutions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data

Method for Calculating Lift Distribtutions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data
Author: James C. Sivells
Publisher:
Total Pages: 722
Release: 1951
Genre: Ailerons
ISBN:

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A method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon lifting-line theory and is an extension to the method described by NACA Report 865. Simplified computing forms containing detailed examples are given for both symmetrical and asymmetrical lift distributions. A few comparisons of experimental and calculated characteristics are also presented.

Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 568
Release: 1965
Genre: Mechanics, Applied
ISBN:

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