A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls / by F.J. Bailey, Jr. and WIlliam J. O'Sullivan.
Flight observations verify theory that increase of rolling acceleration is reduced by increase of hinge movement with air speed, when constant increment of torque is instantly applied to rigid control system having constant moment of inertia and hinge moment coefficient that varies directly with ail...
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| Main Author: | |
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| Corporate Authors: | , |
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| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1942]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L302. |
| Subjects: |
Norlin Library - Basement - Government Information - US
| Call Number: |
Y 3.N 21/5:11/L302
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| Y 3.N 21/5:11/L302 | Available Place a Hold |