机译:环形燃烧器扇形试件中等离子燃烧的地面验证实验
94655 Unit of Chinese People's Liberation Army, Wuhu, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;
Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;
Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China,Research Institute of Army Aviation, Beijing, China;
Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;
Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;
Air Force Engineering University, Xi'an, China,Engineering Department Science and Technology on Plasma Dynamics Laboratory, Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an, China;
机译:航空航天发动机燃烧器的等离子体辅助点火和燃烧进展
机译:航空发动机燃烧室中电介质阻挡放电等离子体辅助燃烧的实验研究
机译:同轴喷射燃烧器中等离子体辅助点火和燃烧的大型涡流模拟
机译:通过新建立的全环形燃烧器测试装置验证简单的一次浓燃烧燃烧方法的低NOx性能
机译:液体火箭发动机燃烧室的疲劳寿命预测与子尺度测试验证。
机译:验证星型跟踪仪的斜率公差的地面测试策略
机译:模拟燃烧试验,用于验证液体火箭燃烧器中最佳阻尼特性的挡板间隙
机译:用于固定式燃气轮机发动机的先进燃烧系统:第三卷。燃烧器验证测试