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.

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http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1660.pdf