1. Ablation With Ice Model at M = 5.8
2. Weiss, R. "Sublimation of a Hemisphere in Supersonic Flow/' TR 391, July 1959, MIT Naval Supersonic Lab.: also TN-59-870, Air Force Office of Scientific Research.
3. Lees, L. "Convective Heat Transfer with Mass Addition and Chemical Reactions/' Combustion and Propulsion, Third AGARD Colloquium, Pergamon Press, New York, 1958, pp.451-498.