Abstract

Turbulent burning velocities for methane/air mixtures at pressures ranging from atmospheric pressure up to 1.0 MPa and mixture temperatures of 300 and 573 K were measured, which covers the typical operating conditions of premixed-type gas-turbine combustors. A bunsen-type flame stabilized in a high-pressure chamber was used, and OH-PLIF visualization was performed with the pressure and mixture temperature being kept constant. In addition to a burner with an outlet diameter of 20 mm for the high-pressure experiments, a large-scale burner with an outlet diameter of 60 mm was used at atmospheric pressure to extend the turbulence Reynolds number based on the Taylor microscale, R λ , as a common parameter to compare the pressure and temperature effects. It was confirmed that R λ over 100 could be attained and that u′/ S L could be extended even at atmospheric pressure. Based on the contours of the mean progress variable 〈 c〉 = 0.1 determined using OH-PLIF images, turbulent burning velocity was measured. S T/ S L was also found to be greatly affected by pressure for preheated mixtures at 573 K. The bending tendency of the S T/ S L curves with u′/ S L was seen regardless of pressure and mixture temperature and the R λ region where the bending occurs corresponded well to the region where the smallest scale of flame wrinkling measured as a fractal inner-cutoff approaches the characteristic flame instability scale and becomes almost constant. A power law of S T/ S L with ( P/ P 0)( u′/ S L) was clearly seen when S T was determined using 〈 c〉 = 0.1 contours, and the exponent was close to 0.4, indicating agreement with the previous results using the mean flame cone method and the significant pressure effects on turbulent burning velocity.

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