42 Publications (Page 2 of 2)
1996
Cold-flow study of hybrid rocket motor flow dynamicsJenkins, Rhonald M⋅Cruit, W. D and Smith, A. WAIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 32nd, Lake Buena Vista, FL; UNITED STATES; 1-3 July 1996. 1996.
| Conference Proceeding
1995
Analysis of ignition and flame spreading in solid rocket motor star slotsCiucci, A.⋅Jenkins, Rhonald M and Foster, Winfred AJournal of Propulsion and Power (0748-4658), vol. 11, (no. 6), pp. 1371-1373, 1995.
| Journal Article
A preliminary analysis of low frequency pressure oscillations in hybrid rocket motorsJenkins, Rhonald M and Cook, J. RAIAA, ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 31st, San Diego, CA; UNITED STATES; 10-12 July 1995. 1995.
| Conference Proceeding
Unsteady jet plume interaction in multi-port SRM ignition systemsJenkins, Rhonald M⋅Foster, Winfred A and Wirth, Lora SAIAA, Aerospace Sciences Meeting and Exhibit, 33rd, Reno, NV; UNITED STATES; 9-12 Jan. 1995. 1995.
| Conference Proceeding
1994
Preliminary design of a space propulsion system utilizing stored thermal energyWilliams, George J⋅Jenkins, Rhonald M and Rose, M. FJournal of Propulsion and Power, vol. 10, (no. 1), pp. 32-39, 1994.
| Journal Article
Simplified model for calculation of backflow contamination from rocket exhausts in vacuumJenkins, Rhonald M⋅Ciucci, Alessandro and Cochran, John EAIAA Paper 90-1846. See accession A90-40529, Journal of Spacecraft and Rockets (0022-4650), vol. 31, (no. 2), pp. 265-270, 1994.
| Journal Article
1993
A semi-empirical model for heat transfer and flame spreading in slotted rocket motorsJenkins, Rhonald M⋅FOSTER, W. A and HENGEL, J. EAIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit, 29th, Monterey, CA; UNITED STATES; 28-30 June 1993. 1993.
| Conference Proceeding
Ignition transient calculations in the Space Shuttle solid rocket motorJenkins, Rhonald M and Foster, Winfred AIn NASA. Marshall Space Flight Center, Eleventh Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1 p 571-595 (SEE N95-23615 07-34). 1993.
| Conference Proceeding
1988
Investigation of open cycle H2-O2 Ljungstrom turbine configurations for space power conversionJenkins, Rhonald M and Skvorz, Sandra JSpace structures, power, and power conditioning; Proceedings of the Meeting, Los Angeles, CA; 11-13 Jan. 1988. 1988.
| Conference Proceeding
1985
Regionally averaged endwall heat transfer correlations for a linear vane cascadeKUMAR, G. N⋅Jenkins, Rhonald M and SAHU, U.ASME, International Gas Turbine Conference and Exhibit, 30th, Houston, TX; UNITED STATES; 18-21 Mar. 1985. 1985.
| Conference Proceeding
1983
A comprehensive method for preliminary design optimization of axial gas turbine stages. II - Code verificationJenkins, Rhonald MAIAA, SAE, and ASME, Joint Propulsion Conference, 19th, Seattle, WA; United States; 27-29 June 1983. 1983.
| Conference Proceeding
1982
A comprehensive method for preliminary design optimization of axial gas turbine stagesJenkins, Rhonald MAIAA, SAE, and ASME, Joint Propulsion Conference, 18th, Cleveland, OH; United States; 21-23 June 1982. 1982.
| Conference Proceeding
1969
A UNIFIED TREATMENT OF METAL OXIDE PARTICLE GROWTH HISTORIES IN ROCKET CHAMBERS AND NOZZLES (Dissertation)Jenkins, Rhonald M (1969).
Ramjet powered missile design using a genetic algorithmHartfield, Roy J⋅Jenkins, Rhonald M and Burkhalter, John E42nd AIAA Aerospace Sciences Meeting and Exhibit; Reno.
| Journal Article
University propulsion programs at Auburn UniversityFoster Jr., Winfred A⋅Hartfield, Roy J and Jenkins, Rhonald M40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit; Fort Lauderdale.
| Journal Article
