Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60 / F.E. West, Jr., and T. Himka.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	West, F. E.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Himka, T.
Other title:	Technical report archive and image library.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1877.
Subjects:	Aerofoils. Lift (Aerodynamics) Pitching (Aerodynamics) Wind tunnel testing.

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Call Number:	Y 3.N 21/5:6/1877
Y 3.N 21/5:6/1877	Available Place a Hold