Charles E. Watkins
naca-tn-2457
Sep 1951
This analysis treats the air forces and moments in supersonic potential flow on oscillating triangular wings and a series of swept-back and arrow wings with subsonic leading edges and supersonic trailing edges. For the wings undergoing sinusoidal torsional oscillations simultaneously with vertical translations, the linearized velocity potential is derived in the form of a power series in terms of a frequency parameter.
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