1. H. T. Nagamatsu and R. E. Sheer, Jr., “Hypersonic shock wave-boundary layer interaction and leading edge slip” (submitted for publication in J. Am. Rocket Soc.).
2. The Free Molecule Probe and Its Use for the Study of Leading Edge Flows
3. E. H. Kennard,Kinetic Theory of Gases(McGraw-Hill Book Company, Inc., New York and London, 1938).
4. R. Schamberg, “The fundamental differential equatons and boundary conditions for high speed flow,” Thesis, California Institute of Technology, (1947).