Formulas and Charts for the Supersonic Lift and Drag of Flat
Swept-Back Wings with Interacting Leading and Trailing Edges.
NACA Technical Note 2093, May 1950.
Cohen, Doris; and Friedman, Morris D.:
Theoretical Investigation of the Supersonic Lift and Drag of Thin,
Sweptback Wings with Increased Sweep Near the Root.
NACA Technical Note 2959, June 1953.
Use of Source Distributions for Evaluating Theoretical Aero-dynamics
of thin Finite Wings at Supersonic Speeds.
NACA Report 951, 1950.
Jones, Robert T.; and Cohen, Doris: High Speed Wing Theory. Princeton.
Puckett, A.E.: Supersonic Wave Drag of Thin Airfoils.
Journal of the Aeronautical Sciences, Vol. 13, 1946, pages 475-484.
Puckett, A.E. and Stewart, H.J., Aerodynamic Performance of Delta Wings at Supersonic Speeds,
Journal of the Aeronautical Sciences, Vol. 14, No. 10, October 1947, pages 567-578.
Charts for the Computation of Lift and Drag of Finite Wings at Supersonic Speeds.
Douglas Aircraft Company Report SM-13480, 14 October 1949.
Puckett, A. E., Supersonic Wave Drag of Thin Airfoils.
Ph.D. thesis at California Institute of Technology, 1949, pages 74-78.
Royal Aeronautical Society Data Sheets, "Aerodynamics," Vol. 2, page Wings S. 00.03.04, August 1956.
Bishop, R.A.; and Cane, E.G.:
Charts of the Theoretical Wave Drag of Wings at Zero Lift.
Current Papers No. 313, Aeronautical Research Council,
[Technical Note Aero. 2421, Royal Aircraft Establishment, June 1956].
A Technique for Improving the Predictions of Linearized Theory on the Drag
of Straight-Edged Wings.
Current Papers No. 394, Aeronautical Research Council, 1958.
[Technical Note Aero. 2474, Royal Aircraft Establishment, January 1957].