1997
DOI: 10.2514/2.5154
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Properties of Laminar Premixed CO/H/Air Flames at Various Pressures

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Cited by 135 publications
(48 citation statements)
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“…This could be attributed to the higher hydrogen content in PG3. This behaviour was also observed by Hassan et al [10]; with an increase of H 2 fraction (by volume) from 3% to 50% in a binary fuel mixture of H 2 -CO, the neutral stability shifts from φ ≈ 1.1 to 1.6, showing the effect of hydrogen content in fuel on preferential diffusion stability.…”
Section: Burning Velocities and Markstein Numbers Of Producer Gas-airsupporting
confidence: 80%
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“…This could be attributed to the higher hydrogen content in PG3. This behaviour was also observed by Hassan et al [10]; with an increase of H 2 fraction (by volume) from 3% to 50% in a binary fuel mixture of H 2 -CO, the neutral stability shifts from φ ≈ 1.1 to 1.6, showing the effect of hydrogen content in fuel on preferential diffusion stability.…”
Section: Burning Velocities and Markstein Numbers Of Producer Gas-airsupporting
confidence: 80%
“…The thermal diffusion effect was included in these computations [14]. Predictions of unstretched laminar burning velocities for these mixtures with RUN1DL using the Warnatz C1 mechanism for spherically expanding flames are plotted in Figure 2 and compared with spherically expanding flame measurements by Hassan et al [10], McLean et al [20], and Sun et al [21] and those obtained with PREMIX using GRI-MECH Hassan et al [10] McLean et al [20] Sun et al [21] RUN1DL-C1 chemistry PREMIX-GRIMECH H 2 50%-CO 50% H 2 5%-CO 95% 3.0 for freely propagating planar flames. The comparisons with experiments are quite good and RUN1DL predicts peak burning velocities at the same equivalence ratios as in the experiments.…”
Section: Assessment Of Suitability Of Reaction Mechanisms For Presentmentioning
confidence: 99%
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“…Groff [4] first measured spherical flame speeds at high pressures, up to 5 atm, by directly imaging the propagating flame front and also through pressure measurements. Lately, Taylor and coworkers [5][6][7] and Faeth and coworkers [8][9][10][11][12][13] determined val-0 s u ues for various fuel compositions and pressures through systematic subtraction of stretch effects using similar imaging techniques. The values so de-0 s u termined, with different stretch-compensated relations, are in reasonably good agreement with each other, as well as with computational calculations and the data from counterflow experiments.…”
Section: Introductionmentioning
confidence: 99%
“…Figure 2 shows the measured laminar burning velocity of H 2 /CO/air mixtures compared with those of previous studies [42,[47][48][49][50][51][52]; all the data were measured with a spherically propagating flame at P u = 0.1 MPa and all data are in good agreement. This proves the correctness of the data obtained in this investigation.…”
Section: System Validation and Laminar Burning Velocitymentioning
confidence: 61%