Estimation of forces and moments due to rolling for several slender-tail configurations at supersonic speeds

Percy J. Bobbitt, Frank S. Malvestuto, Jr.
naca-tn-2955
Jul 1953


The velocity potentials, span loadings, and corresponding force and moment derivatives have been theoretically evaluated for a number of slender-tail arrangements performing a steady rolling motion at supersonic speeds. The method of analysis is based upon an application of conformal-transformation techniques.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1953/naca-tn-2955.pdf