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机译:状态观测器间接测量超燃冲压发动机内壁温度的方法
Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;
Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;
Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;
Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;
Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;
Harbin Inst Technol, Sch Energy Sci & Engn, Harbin 150001, Heilongjiang, Peoples R China;
Indirect online measurement; Inner wall temperature; Scramjet combustor; Mathematical model; Proportional integral observer;
机译:船首推进器在码头墙壁上引起的压力场的全尺寸测量-间接监测海床速度的方法
机译:通过多项式混沌观测器进行间接测量
机译:使用Scramjet进气流量传感器进行亚音速飞行中的温度和压力测量
机译:壁温和湍流建模的超燃冲压发动机进气参数研究
机译:使用冲击回波法在高温环境以及热和材料性能梯度中测量耐火墙厚度。
机译:用于Scramjet流动中壁剪应力测量的高温MEMS表面栅栏
机译:用于超燃冲压发动机壁面剪应力测量的高温mEms表面栅