Calculated effects of geometric dihedral on the low-speed rolling derivatives of swept wings

M. J. Queijo, Byron M. Jaquet
naca-tn-1732
Oct 1948


A simple theory has been used to determine the effects of geometric dihedral angle on the rolling derivatives of swept wings. Equations and charts are given to show these effects.

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http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1732.pdf