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Flame quenching process in cavity based on model scramjet combustor

Flame quenching process in cavity based on model scramjet combustor
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摘要 The flame quenching process in combustors was observed by high speed camera and Schlieren system, at the inflow conditions of Ma = 2.64, To = 1483K, P0 = 1.65 MPa, T = 724 K and P -- 76.3 kPa. Changing process of the flame and shock structure in the combustor was clearly observed. The results revealed that the precom- bustion shock disappeared accompanied with the process in which the flame was blown out and withdrawed from the mainflow into the cavity and vanished after a short while. The time of quenching process was extended by the cavity flame holder, and the ability of flame holding was enhanced by arranging more cavities in the downstream as well. The flame was blown from the upstream to the downstream, so the flame in the downstream of the cavity was quenched out later than that in the upstream. The flame quenching process in combustors was observed by high speed camera and Schlieren system, at the inflow conditions of Ma = 2.64, To = 1483K, P0 = 1.65 MPa, T = 724 K and P -- 76.3 kPa. Changing process of the flame and shock structure in the combustor was clearly observed. The results revealed that the precom- bustion shock disappeared accompanied with the process in which the flame was blown out and withdrawed from the mainflow into the cavity and vanished after a short while. The time of quenching process was extended by the cavity flame holder, and the ability of flame holding was enhanced by arranging more cavities in the downstream as well. The flame was blown from the upstream to the downstream, so the flame in the downstream of the cavity was quenched out later than that in the upstream.
出处 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2012年第1期73-78,共6页 力学学报(英文版)
基金 supported by the National Natural Science Foundation of China (10902124)
关键词 Flame quenching process Cavity Model scramjet combustor Flame quenching process Cavity Model scramjet combustor
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参考文献10

  • 1Ben-Yakar, A., Hanson, R.K.: Cavity flameholders for ignition and flame stabilization in scramjets: review and experimental study. AlA A 98-3122 (1998).
  • 2Lin, K.e., Tam, C.J., Boxx, I., et al.: Flame characteristics and fuel entrainment inside a cavity flame holder in a scramjet combustor. AIAA 2007-5381 (2007).
  • 3Brandstetter, A., Rocci Denis, S., Kau, H.P., et al.: Flame stablization in supersonic combustion. AIAA 2002-5224 (2002).
  • 4Rasmussen, C.e., Driscoll, J.F., Hsu, K.Y., et al.: Blowout limits of supersonic cavity-stabilized flames. AIAA 2004-3660 (2004).
  • 5Jeong, E.J., Byrne, S.O., Jeung, 1S., et al.: Cavity flame-holder experiments in a model scramjet engine. AlAA 2006-7918 (2006).
  • 6Whitehurst, R.B., Krauss, R.H., McDaniel, J.e.: Parametric and time resolved stdies of autoignition and flameholding in a clean-air supersonic combustor. AIAA 92-3424 (1992).
  • 7Meng, D.: Investigation on the supersonic combustion based on the cavtiy flame holders. [Ph.D. Thesis], Chaogsha, China: National University of Defense Technology, 2005 (in Chinese).
  • 8Pan, Y.: Research on the combustion and flow process in the scramjet multi-cavity combustor. [Ph.D. Thesis], Changsha, China: National University of Defense Technology, 2007 (in Chinese).
  • 9Ezekoye, O.A., Greif, R.: A comparison of one and two dimensional flame quenching: heat transfer results. U.S. Department of Energy under Contract No. DE-AC03-76sfO0098.
  • 10Samaniego, J.M.: Stretch-induced quenching in flame-vortex interactions. Center for Turbulence Research Annual Research Brief N94-24156 (1993).

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