1. Euler solutions of the body vortices of tangent ogive cylinders at high angles of attack and supersonic speeds
2. Jorgensen, Leland H., and Perkins, Edward W. "Investigation of Some Wake Vortex Characteristics of an Inclined Ogive-Cylinder Body at Mach Number 2," NACA Report 1371, 1958.
3. Pitts, William C., Nielsen Jack N., and Kaattari, George E. "Lift and Center of Pressure of Wing-Body-Tail Combinations at Subsonic, Transonic, and Supersonic Speeds," NACA Report 1307, 1959.