References ^ack, L. M., "Boundary-Layer Stability Theory," Jet Propulsion Lab., Document 900-277, Rev. A, Pasadena, CA, 1969. Shaw, S. J., and Duck, P. W., "The Inviscid Stability of Supersonic Flow Past Heated or Cooled Axisymmetric Bodies," Physics of Fluids A, Vol. 4, No. 7, 1992, pp. 1541-1557. Mack, L. M., "Effect of Cooling on Boundary-Layer Stability at Mach Number 3," Instabilities and Turbulence in Engineering Flows, edited by D. E. Ashpis, T. B. Gatski, and R. Hirsh, Kluwer Academic, Norwell, MA, 1993, pp. 175-188. Lysenko, V. L, "The Role of the First and Second Modes in Compressible Boundary-Layer Transition," Applied Dynamics, 1986, pp. 809-812. Lin, C. C., The Theory of Hydrodynamic Stability, Cambridge Univ. Press, Cambridge, England, UK, 1955. Mack, L. M., "Linear Stability Theory and the Problem of Supersonic Boundary-Layer Transition," AIAA Journal, Vol. 13, No. 3, 1975, pp. 278-289. Arnal, D., Vignau, F, and Laburthe, F., "Recent Supersonic Transition Studies with Emphasis on the Swept Cylinder Case," Boundary Layer Transition & Control, Proceedings of the Boundary Layer Transition and Control Conference (Cambridge, 1991), Royal Aeronautical Society, ISBN 0903409860,1991.