Two-dimensional wind-tunnel investigation of an NACA 64-009 airfoil with two types of leading-edge flap / Felicien F. Fullmer, Jr.

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Bibliographic Details
Main Author:	Fullmer, Felicien 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, 1948.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1624.
Subjects:	Aerofoils. Flaps (Airplanes) Leading edges (Aerodynamics) Trailing edges (Aerodynamics) Lift (Aerodynamics) Wind tunnel testing.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/1624
Y 3.N 21/5:6/1624	Available Place a Hold