Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8056086 | Acta Astronautica | 2016 | 4 Pages |
Abstract
A reaction mechanism with quantum correction is used to model low-temperature/high-pressure autoignition of lean hydrogen-air mixtures. This approach provides a good approximation for experimental data on autoignition delay and the low activation energy observed in experiments. Calculated results demonstrate that ignition delay time is inversely proportional to pressure, squared. The proposed scaling reduces spread in experimental data. The application of a quantum correction to hydrogen oxidation provides a basis for developing a general reaction mechanism that can be used to predict the autoignition behavior of hydrogen over an entire temperature/pressure range relevant to rocket engine conditions.
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Authors
S.P. Medvedev, G.L. Agafonov, S.V. Khomik,