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dc.contributor.advisorArunan, E
dc.contributor.authorDhoke, Kunal V
dc.date.accessioned2022-06-21T10:25:30Z
dc.date.available2022-06-21T10:25:30Z
dc.date.submitted2021
dc.identifier.urihttps://etd.iisc.ac.in/handle/2005/5759
dc.description.abstractDicyclopentadiene (DCPD), a homodimer of cyclopentadiene (C5H6) was chosen for the present study. DCPD can be obtained by dehydrogenation of JP-10 (jet propellant C10H16) which is currently used as aviation fuel. The combustion chemistry for JP-10 is well established. Very few studies are present in the literature on the thermal decomposition of dicyclopentadiene. Hence, to begin with, the thermal decomposition of DCPD was carried out in a single pulse shock tube. The shock tube is incorporated with the step size driver insert to correct the non-ideal pressure rise due to non-ideal effects. Hence it facilitates the near-ideal behavior behind the reflected shock wave region. The experiments were performed behind the reflected shock wave in the temperature range of 1250-1550 K and pressure range of 13-16 atm. Also, Ab-initio calculations were carried out to find the minimum energy pathway that can lead to the formation of observed products. Thereupon the detailed kinetic modeling was carried out to simulate the concentration profile of different observed products. Ab-initio calculations were carried for the dissociation reaction of dicyclopentadiene to cyclopentadiene conversion. Quantum theory of atoms in molecule (QTAIM) which is based upon electron density topology provides insight into the reaction. AIM analysis along the reaction coordinate was carried out which provides information about bond breaking and bond making phenomenon occurring during chemical transformation. In addition, AIM analysis was used to identify the various types of non-covalent interactions present in the structures along the reaction coordinate from reactant to product. Ignition delays were measured for DCPD using the modified chemical shock tube (CST3) to characterize it as a fuel. The measurement of ignition delay times were performed for three different equivalent ratios 0.5, 1, and 1.5. A comparison of ignition delay times between JP-10 and DCPD has been made. Furthermore, a detailed kinetic mechanism was developed for a better understanding. In addition, a comparison was made between the calculated and experimental observed ignition delay times.en_US
dc.language.isoen_USen_US
dc.rightsI grant Indian Institute of Science the right to archive and to make available my thesis or dissertation in whole or in part in all forms of media, now hereafter known. I retain all proprietary rights, such as patent rights. I also retain the right to use in future works (such as articles or books) all or part of this thesis or dissertationen_US
dc.subjectShock tubeen_US
dc.subjectPyrolysisen_US
dc.subjectQTAIMen_US
dc.subjectQuantum theory of atoms in moleculeen_US
dc.subjectNCIen_US
dc.subjectIgnition delayen_US
dc.subject.classificationResearch Subject Categories::NATURAL SCIENCES::Chemistry::Physical chemistryen_US
dc.subject.classificationResearch Subject Categories::NATURAL SCIENCES::Chemistry::Inorganic chemistryen_US
dc.titleShock Tube Investigation and Modeling of Dicyclopentadiene: Fundamental to Applicationen_US
dc.typeThesisen_US
dc.degree.namePhDen_US
dc.degree.levelDoctoralen_US
dc.degree.grantorIndian Institute of Scienceen_US
dc.degree.disciplineFaculty of Scienceen_US


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