The theoretical characteristics of triangular-tip control surfaces at supersonic speeds Mach lines behind trailing edges

Julian H. Kainer, Mary Dowd King
naca-tn-2715
Jul 1952


Charts are presented for the deflection characteristics for configurations having the sweep of the wing and control-surface trailing edges equal and for the location of the hinge line for balanced controls. Tables of calculations are given for configuration in which the wing and flap trailing edges are unequally swept.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-tn-2715.pdf