Multi-pulse detonation experiments with propane-oxygen

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Farinaccio, R ^a   Harris, P G ^a   Stowe, R A ^a   Akbar, R ^b   LaRochelle, E ^c  

^a DEFENCE RESEARCH AND DEVELOPMENT CANADA VALCARTIER   (Canada)

^b Propulsion Group   (Canada)

^c Numérica Ltée   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AC MOTORS; AUTOMOBILE ENGINES; COMBUSTION; CYLINDER HEADS; IGNITION SYSTEMS; JET ENGINES; MIXTURES; OXYGEN; PLANT SHUTDOWNS; PLASMA JETS; PROPANE; PROPULSION; PULSE DETONATION ENGINES;

CYCLE FREQUENCIES; DESIGN CONSTRAINTS; DETONATION INITIATION; ENERGY PER PULSE; FUEL-AIR MIXTURES; INTERNAL DIAMETERS; NITROGEN DILUTION; THRUST MEASUREMENT;

COMBUSTION KNOCK;

EID: 85086617568     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4070     Document Type: Conference Paper

References (7)

1. Schauer, Fred, Stutrud, Jeff and Bradley, Royce, AIAA Paper 2001-1129, 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 2001.
2. Harris, P. G., Farinaccio, R. Stowe, R. A., Higgins, A. J., Thibault, P. A., and Laviolette J. P., The Effect of DDT Distance on Impulse in a Detonation Tube, AIAA paper 2001-3467, 37th Joint Propulsion Conference and Exhibit, Salt Lake City, Utah, July 2001.
3. Helman, et al., "Experimental Investigation of the Detonation Pulse Engine, " Contractor Report NPS67-85-014CR, Naval Postgraduate School, Monterey, California, September, 1985.
4. Helman, D., Shreeve, R. P. and Eidelman, S., "Detonation Pulse Engine, " AIAA 86-1683, 22nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Huntsville, 1986.
5. Eidelman, S. and Grossmann, W., "Pulsed Detonation Engine Experimental and Theoretical Review, " AIAA 92-3168, 28th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Nashville, 1992.
6. Cooper, M., Jackson, S. and Shepherd, J. E., "Effect of Deflagration-to-Detonation Transition on Pulse Detonation Engine Impulse, " Explosion Dynamics Laboratory Graduate Aeronautical Laboratories, California Institute of Technology, May 30, 2000.
7. Wintenberger, E., Austin, J. M., Cooper, M., Jackson S., and Shepherd, J. E., An Analytical Model for the Impulse of Single-Cycle Pulse Detonation Engine, 37th Joint Propulsion Conference and Exhibit, Salt Lake City, Utah, July 2001.