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  1. Rogers, Arthur W.: Wave Drag of Arrow Wings with Modified Double-Wedge Section. Hughes Aircraft Company Technical Memorandum No. 568, 1 July 1958.
  2. 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.
  3. Cohen, Doris: The Theoretical Lift of Flat Swept-Back Wings at Supersonic Speeds. NACA Technical Note 1555, March 1948.
  4. 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.
  5. 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.
  6. Sward, J.C.: Use of Source Distributions for Evaluating Theoretical Aero-dynamics of thin Finite Wings at Supersonic Speeds. NACA Report 951, 1950.
  7. Jones, Robert T.; and Cohen, Doris: High Speed Wing Theory. Princeton.
  8. Puckett, A.E.: Supersonic Wave Drag of Thin Airfoils. Journal of the Aeronautical Sciences, Vol. 13, 1946, pages 475-484.
  9. 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.
  10. 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.
  11. Puckett, A. E., Supersonic Wave Drag of Thin Airfoils. Ph.D. thesis at California Institute of Technology, 1949, pages 74-78.
  12. Royal Aeronautical Society Data Sheets, "Aerodynamics," Vol. 2, page Wings S. 00.03.04, August 1956.
  13. 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].
  14. 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].
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