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REPORT DATE (DD-MM-YYYY)
2308/BX5f. WORK UNIT NUMBER
PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES)Princeton University Department of Mechanical and Aerospace Engineering Princeton, NJ 08544 8. PERFORMING ORGANIZATION REPORT NUMBER
SPONSORING / MONITORING AGENCY NAME(S) AND ADDRESS(ES)AFOSR/NA 110 Duncan Avenue, Room B115 Boiling AFB, DC 20332-8050
SPONSOR/MONITOR'S ACRONYM(S)
SPONSOR/MONITOR'S REPORT NUMBER(S)
DISTRIBUTION / AVAILABILITY STATEMENTApproved for public release, distribution is unlimited
SUPPLEMENTARY NOTES
01914. ABSTRACT -Present and anticipated variation in jet propulsion fuels due to advanced engine compression ratios and airframe cooling requirements necessitate greater understanding of chemical phenomena associated with the feed system and combustion aspects of the airbreathing propulsion systems under consideration by the U.S. Air Force. With AFOSR support an integrated, fundamental research program had been established at Princeton. The focus during the subject period was directed to understanding the pyrolysis and combustion of endothermic fuels under subcritical conditions and the pyrolysis of these fuels under supercritical conditions. Main consideration was given to methylcyclohexane, decalin and tetralin, which are not only endothermic fuels, but alkylcyclohydrocarbons, the naphthene components of JP fuels. The subcritical conditions in the study were 0.1 MPa (1 atm) and temperatures ranging between 900-1200 K. The supercritical conditions were between 4-9 MPa (40-90 atm) and 720-820 K. The Princeton Turbulent Flow Reactor was used for the subcrital studies and a newly designed coiled tubular reactor for the supercritical studies. Substantial experimentation and analytical evaluation revealed distinct differences between the subcritical and supercritical results. From the rate of fuel decay under the conditions described, it was determined that, although the activation energies were of the same order, the supercritical (4.5 MPa) pre-exponential factor A was two orders of magnitude greater than the subcritical (0.1 MPa) one. Further, not only were complete scission products of all these ...