Research Article
Effects of LOX Particle Diameter on Combustion Characteristics of a Gas-Liquid Pintle Rocket Engine
Table 4
Comparison of simulation results for different mesh resolutions and designed values.
| | Mesh A | Mesh B | Mesh C | Mesh D | Designed value |
| (MPa) | 1.8226 | 1.7977 | 1.8040 | 1.8015 | 1.8 | (K) | 1695.57 | 1671.62 | 1684.74 | 1679.30 | 1679 | (m/s) | 1125.99 | 1110.58 | 1114.53 | 1112.96 | 1126.36 | (%) | 99.97 | 98.60 | 98.95 | 98.81 | ā |
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