Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. : 2 - Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / M. J. Bamber and R. O. House.

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Bibliographic Details
Main Author:	Bamber, M. J.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	House, Rufus O.
Format:	Government Document Book
Language:	English
Published:	Washington D.C. : National Advisory Committee for Aeronautics, 1939.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 730.
Subjects:	Airplanes > Wings > Testing. Airplanes > Fuselage. Stability of airplanes. Rolling (Aerodynamics) Yawing (Aerodynamics) Wind tunnel testing.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/730
Y 3.N 21/5:6/730	Available Place a Hold