1. Jones, RobertT.: EstimatedLift-DragRatios at Supersonic Speed.NACATN 1350,1947.
2. Madden, Robert T.: Aerodynamic Study of a Wing-Fuselage,Combination Employing a Wing SweptBack63 -InvestigationataMachNumber of 1.53toDeterminetheEffectsofCamberingand 'histing the Wing for Uniform Load at a Lift Coefficientof0.25. NACARMA9C07,1949.
3. Brown, Clinton E.; and Hargrave, L. K.: Investigation of Minimum Drag and Maximum Lift-Drag Ratios of Several Wing-Body CombinationsIncluding a Cambered Triangular Wing at Low Reynolds Numbers and at SupersonicSpeeds. NACATN4020,September 1958 (Supersedes NACA RM L51El1, August1951.)