1. The Transverse Curvature Effect in Compressible Axially Symmetric Laminar Boundary-Layer Flow
2. Laminar Boundary Layer on a Circular Cone in Supersonic Flow at Small Angle of Attack, NACA TN 2521 (1951).
3. Hypersonic Flow Over a Yawed Circular Cone, Graduate Aerospace Labs, California Institute of Technology, Pasadena, Memo. No. 69, (1963).
4. Axisymmetric Viscous Flow Past Very Slender Bodies of Revolution
5. Laminar Boundary Layer on a Cone in Supersonic Flow at Large Angle of Attack, NACA TR 1132 (1953).