Method For Calculating Lift Distribtutions For Unswept Wings With Flaps Or Ailerons By Use Of Nonlinear Section Lift Data

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Method For Calculating Lift Distributions For Unswept Wings With Flaps Or Ailerons By Use Of Nonlinear Section Lift Data

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Author : James C. Sivells
language : en
Publisher:
Release Date : 1951

Method For Calculating Lift Distributions For Unswept Wings With Flaps Or Ailerons By Use Of Nonlinear Section Lift Data written by James C. Sivells and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Aeronautics categories.

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.

Method For Calculating Lift Distribtutions For Unswept Wings With Flaps Or Ailerons By Use Of Nonlinear Section Lift Data

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Author : James C. Sivells
language : en
Publisher:
Release Date : 1951

Method For Calculating Lift Distribtutions For Unswept Wings With Flaps Or Ailerons By Use Of Nonlinear Section Lift Data written by James C. Sivells and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Ailerons categories.

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.

Method For Calculating The Rolling And Yawing Moments Due To Rolling For Unswept Wings With Or Without Flaps Or Ailerons By Use Of Nonlinear Section Lift Data

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Author : Albert P. Martina
language : en
Publisher:
Release Date : 1954

Method For Calculating The Rolling And Yawing Moments Due To Rolling For Unswept Wings With Or Without Flaps Or Ailerons By Use Of Nonlinear Section Lift Data written by Albert P. Martina 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.

Technical Note

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951

Technical Note 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 1951 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.

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.

Comparison Of High Speed Operating Characteristics Of Size 215 Cylindrical Roller Bearings As Determined In Turbojet Engine And In Laboratory Test Rig

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Author : Arthur W. Goldstein
language : en
Publisher:
Release Date : 1952

Comparison Of High Speed Operating Characteristics Of Size 215 Cylindrical Roller Bearings As Determined In Turbojet Engine And In Laboratory Test Rig written by Arthur W. Goldstein and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aerodynamics, Supersonic categories.

Report

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Author :
language : en
Publisher:
Release Date : 1954

Report written by 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 : 1950

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 1950 with Aeronautics categories.

Report National Advisory Committee For Aeronautics

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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1951

Report 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 1951 with Aeronautics categories.