Characteristics of thin triangular wings with constant-chord partial-span control surfaces at supersonic speeds

Warren A. Tucker, Robert L. Nelson
naca-tn-1660
Jul 1948


A theoretical analysis was made of the characteristics of constant-chord partial-span control surfaces on thin triangular wings at supersonic speeds by use of methods based on the linearized theory for supersonic flow.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1660.pdf