Rogers, Arthur W.:
Wave Drag of Arrow Wings with Modified Double-Wedge Section.
Hughes Aircraft Company Technical Memorandum No. 568, 1 July 1958.
Cohen, Doris:
Formulas for the Supersonic Loading, Lift, And Drag of
Flat Swept-Back Wings with Leading Edges Behind the Mach Lines.
NACA Report 1050, March 1950.
Cohen, Doris:
The Theoretical Lift of Flat Swept-Back Wings at Supersonic Speeds.
NACA Technical Note 1555, March 1948.
Cohen, Doris:
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.
Sward, J.C.:
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.
Lapin, Ellis:
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].
Randall, D.G.:
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].