The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动声学方法求解二维线化欧拉方程对阵风与叶栅的干涉噪声进行了数值模拟。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动声学方法求解二维线化欧拉方程对阵风与叶栅的干涉噪声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅的非定常分 离、粘性效应跨音激波对失速颤振的影响成为当前气动弹性力学的 主要难点。
声明:以上、词性分类均由互联网资源自动生成,部分未经过
核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用动声学方法求解二维线化欧拉方程对阵风与叶栅的干涉噪声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅的非定常 离、粘性效应
跨音激波对失速颤振的影响
为当前
动弹性力学的 主要难点。
声明:以上例句、词性类均由互联网资源自动生
,
未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气声学方法求解二维线化欧拉方程对阵风与叶栅的干涉噪声进
值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅的非定常分 离、粘效应
跨音激波对失速颤振的影响成为当前气
力学的 主要难点。
声明:以上例句、词分类均由互联网资源自
生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动声学方法求解二维线化欧拉方程对阵风与干涉噪声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡非定常分 离、粘性效应
跨音激波对失速颤振
成为当前气动弹性力学
主要难点。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动声学方法求解二维线化欧拉方程对阵风与的干涉噪声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振的非定常分 离、粘性效应
跨音激波对失速颤振的
为当前气动弹性力学的 主要难点。
声明:以上例句、词性分类均由互联网资源自动生,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
用计算气动声学方法求解二维线化欧拉方程对阵风与叶栅的干涉噪声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅的非定常分 离、粘性效应跨音激波对失速颤振的影响成为当前气动弹性力学的 主要难点。
声明:以上例、词性分类均由互联网资源自动生成,部分未
工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动方法求解二维线化欧拉方程对阵风与叶栅
干涉
行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅非定常分 离、粘性效应
跨音激波对失速颤振
影响成为当前气动弹性
主要难点。
明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件
观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动声学方法求解二维线化欧拉方程对阵风与叶栅声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅非定常分 离、粘性效应
跨音激波对失速颤振
影响成为当前气动弹性力学
难点。
声明:以上例句、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件观点;若发现问题,欢迎向我们指正。
The gust-cascade interaction noise was numerically simulated using computational aeroacoustics by solving the two-dimensional linearized Euler equations.
采用计算气动声学方法求解二维线化欧拉方风与叶栅的干涉噪声进行了数值模拟。
The main difficulty on the study of aeroelasticity lies in the effects of unsteady separation, shock and viscosity to the stall flutter.
振荡叶栅的非定常分 离、粘性效应跨音激波
失速颤振的影响成为当前气动弹性力学的 主要难点。
声明:以、词性分类均由互联网资源自动生成,部分未经过人工审核,其表达内容亦不代表本软件的观点;若发现问题,欢迎向我们指正。