Abstract
'Drummond, J. P., and Hussaini, M. Y., A Detailed Numerical Model of a Supersonic Reacting Mixing Layer, AIAA Paper 861427, June 1986. Riggins, D. W., and McClinton, C. R., A Computational Investigation of Flow Losses in a Supersonic Combustor, AIAA Paper 90-2093, July 1990. Eklund, D. R., Northam, G. B., andHartfield, R. J., ADetailed Investigation of Staged Normal Injection into a Mach 2 Flow, 27th J ANNAF Combustion Meeting, F. E. Warren Air Force Base, Cheyenne, WY, Nov. 1990. Eklund, D. R., Northam, G. B., and Fletcher, D. G., A Validation Study of the SPARK Navier-Stokes Code for Nonreacting Scramjet Combustor Flowfields, AIAA Paper 90-2360, July 1990. Drummond, G. B., A Two-Dimensional Numerical Simulation of a Supersonic, Chemically Reacting Mixing Layer, NASA TM 4055, Dec. 1988. Hitch, B. D., and Senser, D. W., Reduced H2-O2 Mechanisms for Use in Reacting Flow Simulation, AIAA Paper 88-0732, Jan. 1988.
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