Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections / Robert E. Berggren and Donald J. Graham.

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Bibliographic Details
Main Author:	Berggren, Robert E.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Graham, Donald J.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1954.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 3172.
Subjects:	Aerofoils. Leading edges (Aerodynamics) Lift (Aerodynamics) Drag (Aerodynamics) Wind tunnel testing.

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Call Number:	Y 3.N 21/5:6/3172
Y 3.N 21/5:6/3172	Available Place a Hold