To provide data for use in interceptor aircraft mission analyses, studies made in NACA Lewis icing tunnel, included effect of icing on airfoil section lift, drag, and pitching. See also NACA -- Tech Note 4151, separately indexed.
Aerodynamic effects caused by icing of unswept NACA 65A004 airfoil
NACA -- Tech Note
1958
47 pages
Aufsatz (Zeitschrift)
Englisch
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