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机译:基于递归傅里叶变换的高超声速进气口实时起步预测与检测
Academy of Fundamental and Interdisciplinary Sciences, Harbin Institute of Technology, Harbin, Heilongjiang Province 150001, China,School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, China;
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, China;
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, China;
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, China;
School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, China;
Hypersonic inlet; unstart detection and prediction; recursive Fourier transform;
机译:高超声速进气的失控机理,检测与控制研究进展
机译:简化几何形状的高超声速入口-隔离器流中的未启动检测
机译:简化几何形状的高超声速入口-隔离器流中的启动检测
机译:基于递归傅里叶变换的高超声速进气口实时起步预测与检测
机译:高超声速进气口的启动和关闭。
机译:多模块高超声速进气的起步耦合机理分析
机译:用于耳蜗植入应用的基于PDA的实时递归傅里叶变换实现
机译:X B-70飞行试验数据与入口不启动和嗡嗡声模拟预测的比较