Effects of ignition characteristics and geometry on the performance of a JP-10/O2 fueled pulse detonation engine

Author:

Brophy Christopher1,Netzer Dave1

Affiliation:

1. U.S. Naval Postgraduate School, Monterey, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. [71 Detonation Engines,"AIAA Paper-99-2634, 35'h AIAA Joint Propulsion Conference. Bussing, T., and Pappas, G. "An Introduction to Pulse Detonation Engines,"AIAA Paper94-0263. Dabora,E.K. "Statusof Gaseous DetonationWavesandTheir Rolein Propulsion,"EasternStatesSectionMtg, TheCombustionInstitute, 1994. Cambier,J.L. "Strategiesfor PDE PerformanceOptimization, AIAA Paper97-2743,33'dJointPropulsion Conference. Beals,K. "Foundation of aLong-Term ResearchEffort in Liquid-Spray Detonationsfor Usein aPulse DetonationEngine,"MS Thesis,Naval PostgraduateSchool,June1997. Forster,D. "Evaluation of aLiquid-FueledPulseDetonationEngine Combustor,"MS Thesis,Naval PostgraduateSchool,December1998. [S] Kuo, K., Principles of Combbstion,

2. JohnWiley andSons,1986,pp. 230-

3. pp. 19-36. [lo] Dabora,E.K., et.al."Drop SizeEffects

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