Study Of Combustion Instabilities Research Articles

Monitoring the combustion process in large engines.

References 1 Valentine, R. S., Dean, L. E., and Pieper, J. L., An improved method for rocket engine performance prediction, J. Spacecraft Rockets 3, 1409-1414 (1966). 2 Crisman, P. A., Goldwasser, S. R., and Petrozzi, P. J., A general computer program for calculation of rocket performance parameters of propellants containing the atomic species, C, H, N, F and Cl, Proceedings of the ARS Propellant Thermodynamics and Handling Conference (American Rocket Society, New York, 1960), Special Rept. 12, pp. 293-313. 3 DeLeuze, N. C., Walsh, T. J., and Petrozzi, P. J., Calculation of chemical kinetic losses in a rocket nozzle, AerojetGeneral Corp., Thrust Chamber Engineering Rept. 9642:0046 (January 6, 1966). 4 Pieper, J. L., Dean, L. E., and Valentine, R. S., Mixture ratio distribution—its impact on rocket engine performance, Aerojet-General Corp., Thrust Chamber Engineering Rept. 9642: 0062/Revision B (December 21, 1966). 5 Rupe, J. H., A correlation between the dynamic properties of a pair of impinging streams and the uniformity of mixtureratio distribution in the resulting spray, Jet Propulsion Lab. Progress Rept. 20-209 (March 28, 1956). 6 Beltran, M. R., Breen, B. P., Kosvic, T. C., Sanders, C. F., Hoffman, R. J., and Wright, R. O., Liquid rocket engine combustion instability studies, Dynamic Science Final Report, Contract AF 04(611)-10542, AFRPL-TR-66-125 (July 1, 1966).