Calculation of the Aerodynamic Loading of Flexible Wings of Arbitrary Plan Form and Stiffness PDF Download
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Author: Franklin W. Diederich
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 60
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Book Description
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain stability derivatives of wings and tail surfaces of arbitrary plan form and stiffness. Computing forms, tables of numerical constants required in the analysis, and an illustrative example are included.
Author: Franklin W. Diederich
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 60
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Book Description
A method is presented for calculating the aerodynamic loading, the divergence speed, and certain stability derivatives of wings and tail surfaces of arbitrary plan form and stiffness. Computing forms, tables of numerical constants required in the analysis, and an illustrative example are included.
Author: John P.. Mugler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 486
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1082
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Book Description
Author: W. L. Gray
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 704
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Book Description
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: Alfred Gessow
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 304
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Book Description
Author: Ted L. Lomax
Publisher: AIAA
ISBN: 9781600861185
Category : Airframes
Languages : en
Pages : 306
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 664
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274
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Book Description
Author: John W. Weeton
Publisher:
ISBN:
Category : Chromium
Languages : en
Pages : 652
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Book Description
When compared with most alloys systems for which diffusion data have been previously obtained, the diffusion rates of chromium in alpha cobalt-chromium solid solutions were found to be low.
