1. A simple method of calculating the induced velocity of a monoplane wing. Report No. 111, Aeronautical Research Institute, Tokyo Imperial University, 1934.
2. . Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data. NACA TN-1269, 1947.
3. Some Recent Developments in Airfoil Theory
4. . Nonlinear lifting line theory for predicting stalling instabilities on wings of moderate aspect ratio. CASD NSC-76-001, 1976.
5. Theory of wing span loading instabilities near stall. AGARD CP-204, 1976.