2019
DOI: 10.1016/j.fuel.2019.115667
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Thermal cracking of jet propellant-10 with the addition of a core-shell macroinitiator

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Cited by 23 publications
(9 citation statements)
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“…During the flight of hypersonic vehicles (Mach > 5), the surface temperature of the combustion chamber increases sharply because of severe friction between the vehicles and air . Endothermic hydrocarbon fuels that can serve as both the propellant and coolant have been used to solve the thermal management problems of hypersonic vehicles. They can not only provide a powerful driving force for hypersonic vehicles but also absorb heat through physical and chemical heat sinks. exo -Tetrahydrodicyclopentadiene (Figure a), as a high energy-density hydrocarbon, possessing many advantages, such as suitable flash point, low freezing point, and high heat sink capability, is one candidate of advanced functional fuels. It is usually applied as a single-component jet fuel for volume-limited aviation combustion chambers. However, the application of exo -tetrahydrodicyclopentadiene is limited to a certain extent by its poor properties of fluidity, ignition, and combustion which are related to its relatively high viscosity and high carbon to hydrogen ratio (C/H) …”
Section: Introductionmentioning
confidence: 99%
“…During the flight of hypersonic vehicles (Mach > 5), the surface temperature of the combustion chamber increases sharply because of severe friction between the vehicles and air . Endothermic hydrocarbon fuels that can serve as both the propellant and coolant have been used to solve the thermal management problems of hypersonic vehicles. They can not only provide a powerful driving force for hypersonic vehicles but also absorb heat through physical and chemical heat sinks. exo -Tetrahydrodicyclopentadiene (Figure a), as a high energy-density hydrocarbon, possessing many advantages, such as suitable flash point, low freezing point, and high heat sink capability, is one candidate of advanced functional fuels. It is usually applied as a single-component jet fuel for volume-limited aviation combustion chambers. However, the application of exo -tetrahydrodicyclopentadiene is limited to a certain extent by its poor properties of fluidity, ignition, and combustion which are related to its relatively high viscosity and high carbon to hydrogen ratio (C/H) …”
Section: Introductionmentioning
confidence: 99%
“…HPAMAM was developed as a novel macroinitiator for initiating and promoting the cracking of endothermic hydrocarbons. The effect of the local microenvironment with a high concentration of radicals at high temperatures enables HPAMAM to achieve significant cracking and heat-sink enhancement of hydrocarbon fuels at low addition levels. , Therefore, HPAMAM is key to not only the preparation of high-performance oil-soluble NPs but also the generation of free radicals to further promote fuel cracking. The composite catalysts obtained by encapsulating nanoparticles with hyperbranched poly­(amidoamine) are thus assumed to excel in supercritical cracking of fuels, as depicted in Scheme .…”
Section: Introductionmentioning
confidence: 99%
“…As displayed in Figure c,d, with the addition of 0.10 wt % CBHPG, the conversion and gas yield of n -undecane gradually increase with the rise of the reaction temperature. The increasing molecular weight of CBPHG is beneficial to improving the cracking conversion and gas yield of n -undecane, which is consistent with the phenomenon observed in previous studies . With the existence of CBHPG-3, the conversion and gas yield at 675 °C rise from 60.3 and 32.4 to 70.9 and 44.3%, respectively.…”
Section: Resultsmentioning
confidence: 99%
“…The thermal oxidation deposition and cracking performance of hydrocarbon fuels with CBHPG were evaluated in a tubular reactor which was used to simulate the heat-exchange process of fuels in microchannels of an aircraft engine. The structure of the experimental apparatus is given in Figure , and the details of the cracking experiments can be found in our previous work. , As a kind of superalloy with a maximum operating temperature of 1100 °C, the GH3128 tube (1 m length, 3.0 mm outer diameter, and 2.0 mm inner diameter) was chosen to be the reaction channel. Considering the catalytic effect of metal, the tube was completely passivated at a high temperature (over 800 °C) before the experiment.…”
Section: Methodsmentioning
confidence: 99%
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