1. S. Goldstein,Modern Developments in Fluid Dynamics, 1st ed., vol. 2 (Oxford University Press, London 1938), p. 631.
2. M. Sibulkin,Heat Transfer Near the Forward Stagnation Point of a Body of Revolution, J. aeron. Sci.19, No. 8, 570–571 (August 1952).
3. I. Korobkin,Laminar Heat-Transfer Characteristics of a Hemisphere for Mach Number Range 1–9 to 4–9 (Heat Transfer and Fluid Mechanics Institute, June 23–25, 1955).
4. H. A. Stine andK. Wanlass,Theoretical and Experimental Investigation of Aerodynamic-Heating and Isothermal Heat-Transfer Parameters on a Hemispherical Nose with Laminar Boundary Layer at Supersonic Mach Numbers, NACA TN 3344 (December 1954).
5. E. R. van Driest,The Problem of Aerodynamic Heating, Aeron. Eng. Rev.15, No. 10, 26–41 (October 1956).