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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2020
/
Article
/
Tab 4
/
Research Article
Numerical Analysis of Self-Excited Combustion Instabilities in a Small MMH/NTO Liquid Rocket Engine
Table 4
The comparison of constant-volume combustion theory results and CFD simulation results.
(constant-volume combustion theory)
(CFD simulation)
(MPa)
3.14
4.47
4.58
(K)
2646
3231
3185
(g cm
-3
)
4.93
-
3
4.93
-
3
5.14
-
3