The damping due to roll of triangular, trapezoidal, and related plan forms in supersonic flow

Arthur L. Jones, Alberta Alkene
naca-tn-1548


Within the limitations of linearized potential theory for supersonic flow, solutions have been obtained for the damping in roll of triangular, trapezoidal, rectangular, and two swept-back plan forms.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1548.pdf