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.

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Bibliographic Details
Main Author:	Bailey, F. J.
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors:	O'Sullivan, William J.
Other title:	NACA Wartime Reports. Series L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L302.
Subjects:	Ailerons. Airplanes > Control systems. Rolling (Aerodynamics) Moments of inertia. Mathematics. Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number:	Y 3.N 21/5:11/L302
Y 3.N 21/5:11/L302	Available Place a Hold