1. A Study of Supersonic Combustion;GROSS;Journal of the Aerospace Sciences,1960
2. NICHOLLS, J. A., Stabilized Gaseous Detonation Waves. American Rocket Society Journal, Vol. 29, No. 8, pp. 607–608, August 1959 (Also available in modified form as Ph.D. thesis, University of Michigan 1960, through University Microfilms, Inc., Ann Arbor, Michigan).
3. RHODES, R. D. and CHRISS, D. E., A Preliminary Study of Stationary Shock Induced Combustion with Hydrogen-Air Mixture. AEDC TN 61–36, July 1961.
4. RHODES, R. P., RUBINS, P. M., CHRISS, D. E., The Effect of Heat Release on the Flow Parameters in Shock-induced Combustion. AEDC TDR-62–78, May 1962.
5. OPPENHEIM, A. K., Development and Structure of Plane Detonation Waves. Fourth AGARD Combustion and Propulsion Colloquium, Milan, Italy, pp. 186–258, April 1960; Pergamon Press Ltd., London (1960).