College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics Nanjing, China, Department of Flight Theory Education, PLA the 94580 Unit,Bengbu, China,);
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics Nanjing, China;
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics Nanjing, China;
College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics Nanjing, China;
primary jet; dual-stage swirler; combustor; flow field; piv measurement;
机译:进气涡流和喷雾锥角对燃气轮机燃烧室液体燃料喷雾燃烧和排放性能的影响
机译:旋流和主风量对液化气涡轮燃烧室排放和性能的影响
机译:旋流和主要区域气流率对液体燃气燃气轮机燃烧器排放和性能的影响
机译:初级空气喷射对双级旋流式燃烧器流动和燃烧性能的影响
机译:研究液体射流和预雾化喷雾在有限的旋流中的混合,以实现稀薄的直接喷射燃烧。
机译:部分预混合和热损失对旋流稳定型燃气轮机模型燃烧器反应流场预测的影响
机译:水模型Can型燃烧器中旋流/稀释喷射流动分裂旋流/稀释射流的研究
机译:旋流喷射燃烧器模块的燃烧稳定性极限,结合空气涡流和astm a-1燃料撞击喷射雾化