Wind-tunnel investigation of an N.A.C.A. 23021 airfoil with two arrangements of a 40-percent-chord slotted flap / Frank Duschik.

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Bibliographic Details
Main Author:	Duschik, Frank
Corporate Author:	United States. National Advisory Committee for Aeronautics
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) ; 728.
Subjects:	Aerofoils. Slotted flaps (Airplanes) Wind tunnel testing. Aerodynamics.

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Call Number:	Y 3.N 21/5:6/728
Y 3.N 21/5:6/728	Available Place a Hold