Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Emission Reduction of Fuel-Staged Aircraft Engine Combustor Using an Additional Premixed Fuel Nozzle



    Published in:

    Publication date :

    2013



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    52.52 Thermische Energieerzeugung, Wärmetechnik / 52.30 Strömungskraftmaschinen, Turbomaschinen / 52.52 / 52.30



    Engine Demonstration of NOx Reductions with a Fuel-Staged Gas Turbine Combustor

    Segalman, I. / Smith, R. / Sturgess, G. et al. | British Library Conference Proceedings | 1994


    Engine demonstration of NO(x) reductions with a fuel-staged gas turbine combustor

    Segalman, I. / Smith, R. / Sturgess, G. et al. | AIAA | 1994


    Emission Characteristics of Premixed Lean Diesel Combustion with Extremely Early Staged Fuel Injection

    Keiichi, Nakagome / Keiichi, Niimura / Takeda, Yoshinaka | SAE Technical Papers | 1996


    Kinetic modeling study on the emission characteristics of an axial-fuel-staged MILD combustor

    Zheng, Xianglong / Xiong, Yan / Lei, Fulin et al. | TIBKAT | 2019

    Free access

    Distributed Fuel Injection for Performance Improvement of Staged Supersonic Combustor

    Sadatake Tomioka / Kan Kobayashi / Kenji Kudo et al. | AIAA | 2005