Two-dimensional wind-tunnel investigation of a 10.7-percent-thick symmetrical tail section with a 0.40 airfoil-chord control surface and a 0.20 control-surface-chord tab / Albert L. Braslow.

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Bibliographic Details
Main Author:	Braslow, Albert L.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington D.C. : National Advisory Committee for Aeronautics, 1947.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1228.
Subjects:	Airplanes > Control surfaces. Airplanes > Tail surfaces. Aerofoils. Flaps (Airplanes) Tabs (Airplanes)

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Call Number:	Y 3.N 21/5:6/1228
Y 3.N 21/5:6/1228	Available Place a Hold