A theoretical and experimental investigation of the effects of yaw on pressures, forces, and moments during seaplane landings and planing / Robert F. Smiley.

A theory for the side force, rolling moment, yawing moment, and pressure distribution during yawed landings and planing of seaplanes was developed. For the special case of the straight-sided wedge without chine immersion, the results of the theoretical analysis are presented in the form of generaliz...

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Bibliographic Details
Main Author: Smiley, Robert F.
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2817.
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Call Number: Y 3.N 21/5:6/2817
Y 3.N 21/5:6/2817 Available Place a Hold