angle of sideslip meaning in Chinese
侧滑角
Examples
- The pressure model of flush airdata sensing system is nonlinear equations of the angle of attack , angle of sideslip , dynamic pressure and static pressure of the free stream
飞行器表面的压力分布是大气数据(迎角、侧滑角、动压、静压)的非线性函数,这个函数主要可以从空气动力学模型得到。 - The relevance functions between total pressure recover coefficient and the parameters ( mach number , angle of attack , flow coefficient , angle of sideslip ) for subsonic submerged inlet in turbojet and turbofan engine were investigated
摘要根据某埋入式进气道试验数据建立了计算埋入式亚声速进气道总压恢复系数的经验公式，表现为关于马赫数、流量系数、攻角、侧滑角的函数。 - The formula for mach number has been optimized with least - squres solution , thus the precision of a polynomial of power of 5 is better than that of 9 . 2 . after the solving of angle of attack and angle of sideslip , the theory of general inverse of matrix is used to simplify the nonlinear equations and to calculate the total pressure and the modified dynamic pressure ratio . these two parameters together with the angle of attack and angle of sideslip contain enough information to work out the dynamic pressure and static pressure
其中包括: 1 .应用最小二乘法,对马赫数的泰勒求解公式进行优化,优化后的求解公式采用5次多项式即可在精度上优于原有的9次多项式,可以提高运算速度; 2 .提出应用广义逆矩阵简化非线性方程组:在已经求解出迎角与侧滑角的前提下,直接从原始的压力向量中提取出总压,并且提出了动压修正比的概念。