Table 1. Previous Experimental Studies of Pyrolysis and Combustion of RP-3 Jet Fuel.

year	type of experiment	conditions	type of data	reference
2012	shock tube	T = 820–1500 K; p = 5.5, 11, 22 atm; φ = 0.5, 1.0, 1.5	ignition	Liang et al.43
2015	shock tube	T = 650–1500 K; p = 1–20 atm; φ = 0.2, 1.0, 2.0	ignition	Zhang et al.11
2015	shock tube	T = 1100–1600 K; p = 1, 2, 3 atm; φ = 0.5, 1.0, 1.5	ignition	Zeng et al.38
2015	counterflow flame	T0 = 403 K; p = 1 atm; φ = 0.7–1.4	laminar flame speed	Zheng et al.39
2016	constant volume combustion chamber	T0 = 390, 420, 450 K; p = 1, 3, 5, 7 atm; φ = 0.6–1.6	laminar flame speed	Ma et al.40
2017	shock tube	T = 1670–2200 K; p = 2, 5 atm; φ = 5, 10, 20	soot	He et al.44
2019	shock tube	T = 1113–1600 K; p = 0.1–1 atm; φ = 0.5–1.5	ignition	Chen et al.14
2019	shock tube rapid compression machine	T = 624–1437 K; p = 10, 15, 20 atm; φ = 0.5–1.5	ignition	Mao et al.15
2021	shock tube	T = 920–1590 K; p = 2, 10 atm; φ = 0.5, 1.0, 2.0	ignition	Yang et al.45