Some measurements of aerodynamic forces and moments at subsonic speeds on a wing-tank configuration oscillating in pitch about the wing midchord

Sherman A. Clevenson, Sumner A. Leadbetter
naca-tn-3822
Dec 1956


Measurements are presented of the aerodynamic forces and moments acting on a wing-tank configuration, with or without fins, oscillating in pitch about the wing-root midchord. The reduced-frequency range was from 0.050 to 0.657, whereas the Mach number and Reynolds number ranges were from 0.18 to 0.75 and 0.9 X 10(6) to 9.5 10((6), respectively.

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