The Aerodynamic characteristics of three tapered airfoils tested in the Variable Density Wind Tunnel /
Raymond F. Anderson.

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Main Author: Anderson, Raymond F.
Related Names: United States. National Advisory Committee for Aeronautics.
Language(s): English
Published: Washington D.C. : National Advisory Committee for Aeronautics ; 1931.
Subjects: Moments of inertia.
Drag (Aerodynamics)
Lift (Aerodynamics)
Aerofoils > Aerofoils / Wind tunnel testing.
Summary: This report contains the lift, drag, and moment characteristics of tapered Clark Y, Gottingen 398, and U.S.A. 45 airfoils as obtained from tests made in the Variable Density Wind Tunnel. The results are given at both low and high Reynolds numbers to show scale effect and to provide data for use in airplane design.
Note: NACA TN no. 367.
"February, 1931."
Physical Description: 12, [10] leaves : ill., tables ; 27 cm.
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