Effect of the Primary Hole Parameters on Combustion Performance of Dual-Stage Swirl Model Combustor

Author:

Ren Dongliang,Fan Weijun,Zhang Rongchun

Publisher

Springer Nature Switzerland

Reference17 articles.

1. Dang X, Zhao J-h et al (2007) Experimental study of effects of geometric parameters on combustion performance of dual-stage Swirler combustor. J Aerospace Power 22(10):1639–1645

2. Dang X, Zhao J et al (2008) Effect of main combustion hole on the flow field of dual swirl combustor. J Nanjing Univ Aeronautics Astronautics(01):26–31

3. Dang X, Zhao J et al (2010) Effect of main hole on flow field in model combustor. Propulsion Technol 31(01):24–28

4. EIkady AM (2006) The influence of primary air jets on flow and pollutant emissions characteristics within a model gas turbine combustor. AIAA 2006–544

5. Elkady A, Jeng SM (2006) The influence of primary air jets on flow and pollutant emissions characteristics within a model gas turbine combustor. In: 44th AIAA aerospace sciences meeting and exhibit, p 544

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