Journal of the Combustion Society of Japan
Online ISSN : 2424-1687
Print ISSN : 1347-1864
ISSN-L : 1347-1864
Volume 49 , Issue 149
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FEATURE—The Latest Combustion Technologies of Propulsion Systems for High Speed Flying Objects
ORIGINAL PAPER
  • Kazuhiro YAMAMOTO, Tsutomu ISAYAMA, Naoki HAYASHI, Hiroshi YAMASHITA
    Type: ORIGINAL PAPER
    2007 Volume 49 Issue 149 Pages 181-186
    Published: 2007
    Released: April 13, 2019
    JOURNALS FREE ACCESS

    In this study, we have simulated counterflow premixed flames to discuss burning velocity and OH concentration. Two-types of flow configuration are considered. One is twin premixed flames in symmetric counterflow premixed mixtures. The other is a single-flame in counterflows consisted of premixed mixture and air. The fuel is propane, and the equivalence ratio is 0.7 to 1.0. The detailed chemical kinetics model of GRI-Mech 3.0 using 53 species and 325 reactions is adopted. To change the stretch rate, the inflow velocity is varied from 0.5 to 3.5 m/s. The distance between two inflow boundaries is 15 mm. Based on the reaction rate, we have estimated the burning velocity at different stretch rates. Results show that the burning velocity is decreased with an increase of stretch rate. The burning velocity of the single-flame is smaller than that of twin flames at the same equivalence ratio and stretch rate. The clear relationship between maximum OH concentration in the flame zone and burning velocity is observed especially in the case of single-flame.

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