Research Article

Modified Quasi-Steady Fuel Droplet Combustion Model

Table 3

Proposed model 𝑛 -hexane results.

Iteration 𝑇 𝑓 𝐺 [K] 𝑇 [K] 𝑘 g [W/m K] 𝑐 𝑝 g [kJ/kg K] 𝑇 + [K] 𝑘 + g [W/m K] 𝑐 + 𝑝 𝑔 [kJ/kg K] 𝐿 𝑒 𝐿 𝑒 + 𝑛 𝐴 𝐵 𝑇 𝑓 [K] 𝑟 𝑓 / 𝑟 𝑠 K [ 1 0 3 c m 2 / s ] | 𝑇 𝑓 𝐺 𝑇 𝑓 | [K]

121001221.00.1068722.63181199.00.0771161.17392.800.820.180.9563.432349.111.797.32249.1
22349.11345.60.1148223.08071323.60.0852421.19682.450.770.170.9668.462387.710.957.8338.6
32387.71364.90.1160933.15121342.90.0865861.20032.410.760.160.9669.382394.610.817.916.9
42394.61368.30.1163203.16381346.30.0868271.20102.400.760.160.9669.542395.810.797.921.2

Fixed variables: 𝑇 𝑠 = 𝑇 b o i l = 3 4 2 K , 𝑇 = 2 9 8 K , 𝜌 𝑙 = 6 5 9  kg/ m 3 , Δ 𝑐 = 4 5 0 9 1  kJ/kg, 𝑓 𝑔 = 3 5 5 kJ/kg, 𝜐 = 1 5 . 2 , 𝜒 𝐹 = 0 . 5 5 , 𝜒 𝑂 𝑥 = 0 . 4 5 , 𝑌 𝐹 = 0 . 7 9 , 𝑌 𝑂 𝑥 = 0 . 2 1 .