A Method For Calculating The Subsonic Steady State Loading On An Airplane With A Wing Of Arbitrary Plan Form And Stiffness PDF Download
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Author | : W. L. Gray |
Publisher | : |
Total Pages | : 120 |
Release | : 1995 |
Genre | : |
ISBN | : |
Download A Method for Calculating the Subsonic Steady-state Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness Book in PDF, ePub and Kindle
Author | : W. L. Gray |
Publisher | : |
Total Pages | : 704 |
Release | : 1953 |
Genre | : Aerodynamic load |
ISBN | : |
Download A Method for Calculating the Subsonic Steady-state Loading on an Airplane with a Wing of Arbitrary Plan Form and Stiffness Book in PDF, ePub and Kindle
A method for computing the steady-state span load distribution on an elastic airplane wing for specified airplane weights and load factors is given. The method is based on a modification of the Weissinger L-method and applies at subcritical Mach numbers. It includes the effects of external stores and fuselage on the spanwise loading. Modifications are outlined for treating tail-boom and tailless airplane configurations and for calculating the divergence dynamic pressure of a swept wing with a large external store. A method is also outlined for reducing wind-tunnel data to obtain effective aerodynamic coefficients which are free of model flexibility effects. The effects of Mach number can readily be evaluated from the aerodynamic coefficients thus obtained.
Author | : M. J. Queijo |
Publisher | : |
Total Pages | : 54 |
Release | : 1955 |
Genre | : Aerodynamic load |
ISBN | : |
Download Theoretical Span Load Distributions and Rolling Moments for Sideslipping Wings of Arbitrary Plan Form in Incompressible Flow Book in PDF, ePub and Kindle
A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitrary plan form in incompressible flow is derived. The method requires that the span load at zero sideslip be known for the wing under consideration. Because this information is available for a variety of wings, this requirement should not seriously restrict the application of the present method. The basic method derived herein requires a mechanical differentiation and integration to obtain the rolling moment for the general wing in sideslip. For wings having straight leading and trailing edges over each semispan, the rolling moment equation in terms of plan-form parameters and the lateral center of pressure of the lift due to angle of attack. Calculated span loads and rolling-moment parameters are compared with experimental values. The comparison indicates good agreement between calculations and available experimental data.
Author | : Ted L. Lomax |
Publisher | : AIAA |
Total Pages | : 306 |
Release | : 1996 |
Genre | : Airframes |
ISBN | : 9781600861185 |
Download Structural Loads Analysis Book in PDF, ePub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1038 |
Release | : 1956 |
Genre | : Aeronautics |
ISBN | : |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, ePub and Kindle
Author | : Robert F. Smiley |
Publisher | : |
Total Pages | : 108 |
Release | : 1958 |
Genre | : Aerodynamics |
ISBN | : |
Download Unsteady Aerodynamic Forces on Subsonic Aircraft Exposed to Blast Gusts of Arbitrary Orientation Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 750 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Download A Selected Listing of NASA Scientific and Technical Reports for ... Book in PDF, ePub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 496 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : |
Download Index of NACA Technical Publications Book in PDF, ePub and Kindle
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 692 |
Release | : 1948 |
Genre | : Aeronautics |
ISBN | : |
Download Annual Report of the National Advisory Committee for Aeronautics Book in PDF, ePub and Kindle
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Author | : |
Publisher | : |
Total Pages | : 516 |
Release | : 1968 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle