Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. : 5 - Symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail / by Arthur R. Wallace and Thomas R. Turner.

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Bibliographic Details
Main Author:	Wallace, Arthur R.
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors:	Turner, Thomas R.
Other title:	NACA Wartime Reports. Series L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L459.
Subjects:	Aerofoils. Airplanes > Tail surfaces. Airplanes > Wings. Interference (Aerodynamics) Stability of airplanes, Lateral. Wind tunnel testing. 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/L459
Y 3.N 21/5:11/L459	Available Place a Hold