氣動迎角 的英文怎麼說
中文拼音 [qìdòngyíngjiǎo]
氣動迎角
英文
aerodynamic angle of attack-
Within the field of ground effect, aerodynamic forces of the wing - in - surface effect crafts are not only decided by the angle of attack, but also by the flying height, and they lead to more complicated stability problems
在地效作用區域內，地效飛機的氣動力不僅與迎角有關，而且與飛行高度有關，因而其飛行穩定性問題更為復雜。The shm ( single hole microblowing ) as a new perturbation active control technique has been applied to the slender body with different model noses at zero sideslip and high angle of attack
摘要在亞臨界流動范圍內，對具有不同頭部形狀的尖拱形細長旋成體在無側滑大迎角下進行單孔位微吹氣擾動控制實驗。Aerodynamic angle of incidence
氣動迎角Aerodynamic angle of attack
氣動迎角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
飛行器表面的壓力分佈是大氣數據（迎角、側滑角、動壓、靜壓）的非線性函數，這個函數主要可以從空氣動力學模型得到。In this paper, the boundary layer characteristics of a supercritical airfoil is researched in wind tunnel. from the start to control boundary layer separation and to improve aerodynamics characteristics of this airfoil, three kinds of trapezoid, delta and airfoil shaped vortex generators are designed based on traditional, sub boundary layer and micro - vortex generators conceptual design. it include as follows : 1
研究工作中，從控制該翼型附面層分離、提高大迎角氣動性能的角度出發，通過風洞實驗研究，研究了該翼型的附面層特性和氣動性能，針對其附面層特性，給出了梯形、三角形和翼型式三種渦流發生器設計方案，為下一步研究工作奠定了堅實基礎。On the sensitivity of aircraft longitudinal flying qualities to aerodynamic derivatives at high angle of attack
飛機縱向飛行品質對大迎角氣動導數的敏感性研究The analyses indicate that the shm ' s control ability has strong adaptability to various slender body at high angles of attack, and its control ability is determined by the original state of the flowfield around the slender body
實驗分析表明，單孔位微吹氣擾動這一大迎角非對稱控制手段具有較強的適應能力，其控制能力的大小則由該頭部形狀的初始狀態決定。分享友人