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| Name | stm_3a |  |
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|---|---|---|---|---|
| Target Type | shock tube ignition delay | |||
| Definition | time to d[OH]/dt|max | |||
| Composition | 0.1% H2/0.05% O2/99.85% Ar/80 ppb H | |||
| Temperature T5 (K) | 1524 | |||
| Pressure p5 (atm) | 64 | |||
| Experiment | Trial | Optimized | ||
| Nominal Value (μs) | 46.9 | 44.2 | 46.9 | |
| Uncertainty (σ) | ×/÷ 1.20 | ×/÷ 1.10 | ×/÷ 1.05 | |
| Sensitivity |  |
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| Reference(s) | |
|---|---|
| PDR1996 | Petersen EL, Davidson DF, Röhrig M, Hanson R. High–pressure shock–tube measurements of ignition times in stoichiometric H2/O2/AR mixtures. In: Sturtevant B, Shepherd JE, Hornung HG, editors. Proceedings of the 20th international symposium on shock waves; 1996; Pasadena, California. p. 941–6. |
| UKD2014 | Urzay J, Kseib N, Davidson DF, Iaccarino G, Hanson RK. Uncertainty-quantification analysis of the effects of residual impurities on hydrogen–oxygen ignition in shock tubes. Combust Flame. 2014;161:1-15. |