A Method For Calculating The Subsonic Steady State Loading On An Airplane With A Wing Of Arbitrary Plan Form And Stiffness
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A Method For Calculating The Subsonic Steady State Loading On An Airplane With A Wing Of Arbitrary Plan Form And Stiffness
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Author : W. L. Gray
language : en
Publisher:
Release Date : 1953
A Method For Calculating The Subsonic Steady State Loading On An Airplane With A Wing Of Arbitrary Plan Form And Stiffness written by W. L. Gray and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aerodynamic load categories.
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.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1953
Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aeronautics categories.
Technical Note
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Author :
language : en
Publisher:
Release Date : 1953
Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aeronautics categories.
Theoretical Span Load Distributions And Rolling Moments For Sideslipping Wings Of Arbitrary Plan Form In Incompressible Flow
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Author : M. J. Queijo
language : en
Publisher:
Release Date : 1955
Theoretical Span Load Distributions And Rolling Moments For Sideslipping Wings Of Arbitrary Plan Form In Incompressible Flow written by M. J. Queijo and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aerodynamic load categories.
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.
Structural Loads Analysis
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Author : Ted L. Lomax
language : en
Publisher: AIAA
Release Date : 1996
Structural Loads Analysis written by Ted L. Lomax and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996 with Airframes categories.
Unsteady Aerodynamic Forces On Subsonic Aircraft Exposed To Blast Gusts Of Arbitrary Orientation
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Author : Robert F. Smiley
language : en
Publisher:
Release Date : 1958
Unsteady Aerodynamic Forces On Subsonic Aircraft Exposed To Blast Gusts Of Arbitrary Orientation written by Robert F. Smiley and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1958 with Aerodynamics categories.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Aeronautics categories.
Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1953
Annual Report Of The National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Aeronautics categories.
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1949
A Selected Listing Of Nasa Scientific And Technical Reports For written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aeronautics categories.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1968
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1968 with categories.