Experimental determination of lift and moment on oscillating airfoil; results compared with predictions of vortex sheet theory as described in NACA -- Report 496, 1935; use of theory on aeroelastic problems such as flutter could then be verified or modified. Supersedes NACA -- Tech Note 2465.
Experimental aerodynamic derivatives of sinusoidally oscillating. Airfoil in two-dimensional flow
NACA -- Report
1952
44 pages
Report
English
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