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

Authur L. Jones, John R. Spreiter, Alberta Alksne
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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