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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2018
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Article
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Tab 4
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Research Article
Numerical Investigation of Combustion Characteristics of a Wave Rotor Combustor Based on a Reduced Reaction Mechanism of Ethylene
Table 4
Species and related mass fractions during adiabatic equilibrium phase of ethylene.
Component
Mass fraction
Component
Mass fraction
H
2
0.00334
O
0.0701
H
0.00343
OH
0.0629
CO
2
0.197
H
2
O
0.069
CO
0.197
O
2
0.127