
doi: 10.2514/3.6441
References 1 Davies, L. and Wilson, J. L., "The Influence of Shock and Boundary Layer Interaction on Shock Tube Flows," A.R.C. 29 064-Hyp. 615, May 1967, National Physical Lab., Teddington, England. 2 Lap worth, K. C., The High Temperature Aspects of Hypersonic Flow, AGARDograph 68, Pergamon, N.Y., 1964, pp. 255267. 3 Richmond, J. K. and Parson, R. J., "Driver Gas Contamination in Shock Tunnels," Dl-82-0806, Dec. 1968, Boeing Scientific Research Labs., Seattle, Wash. 4 Bull, D. C. and Edwards, D. H., "An Investigation of the Reflected Shock Interaction Process in a Shock Tube," AIAA Journal, Vol. 6, No. 8, Aug. 1968, pp. 1549-1555. 5 Markstein, G. H., "Flow Disturbances Induced Near a Slightly Wavy Contact Surface, or Flame Front, Traversed by a Shock Wave," Journal of the Aerospace Sciences, Vol. 238, No. 3 March 1958, pp. 238-239. 6 Echigo, R., "Evaluation of Band Emissivities of Carbon Dioxide and Water Vapour," JSME Bulletin, Vol. 10, Aug. 1967, pp. 671-679.
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