The rolling moment due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow

Authur L. Jones, John R. Spreiter, Alberta Alksne
naca-tn-1700
Oct 1948


The rolling moment due to sideslip in supersonic flow has been calculated for a representative group of plan forms. The analysis was based on linearized potential theory and was applied to triangular, trapezoidal, rectangular, and swept-back plan forms without dihedral.

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