tilting rotor造句
例句與造句
- The rotor / wing aerodynamic interactions of the tilt rotor vehicle in hover is described in this dissertation
本文主要研究的是傾轉(zhuǎn)旋翼飛行器懸停狀態(tài)時，旋翼機翼之間的氣動干擾問題。 - A simulation of the guidance scheme applied to the example tilt rotor vehicle exhibits satisfactory behavior in the presence of wind and initial errors
仿真結(jié)果表明,在初始擾動和有風(fēng)作用下,垂直距離偏差均達到很小。 - Thus the flight dynamic characteristics and control features in the conversion mode are the key technologies in the whole tilt rotor design
過渡模式飛機的氣動布局改變主要體現(xiàn)在縱向平面內(nèi),所以本文主要研究過渡模式下飛機縱向通道的動力學(xué)特性和控制系統(tǒng)設(shè)計。 - When the tilt rotor vehicle is in hover , the aerodynamic download of the rotor flowfield imposes on the wing . in this time , the rotor / wing interaction is severe
傾轉(zhuǎn)旋翼飛行器懸停時，旋翼的下洗流剛好作用在機翼上，此時，旋翼機翼間的氣動干擾非常劇烈。 - The model developed here is suitable for the tilt rotor aircraft during hover , transition and cruise . the longitudinal equations of motion provide a foundation for further investigation on tilt - rotor flight dynamics
文中所建模型具有較高精度,適合于飛行包線內(nèi)的所有模式,為傾轉(zhuǎn)旋翼飛機飛行動力學(xué)的進一步研究提供了基礎(chǔ)。 - It's difficult to find tilting rotor in a sentence. 用tilting rotor造句挺難的
- A mathematical model reflecting the tilt rotor unsteady and nonlinear aerodynamic characteristics in the longitudinal channel is presented in the paper . in the full flight envelope , the rotor thrust continues tilting and the aerodynamic forces of each component change as a function of airspeed and nacelle angle
在整個飛行包線內(nèi),旋翼的推力矢量方向不斷變化,飛機各部件的氣動力隨發(fā)動機短艙傾角和空速的變化而變化,因而飛機的飛行動力學(xué)有很強的非定常、非線性特性。 - Variable diameter rotor is an effective method to improve the aerodynamic performance of tilt - rotor in both hover and cruise state . on the basis the research before , the variable diameter tilt rotor structure design has been finish , and in virtue of the technology of virtual prototyping to simulate and analyze the kinetic , dynamic and intensity property of it
變直徑傾轉(zhuǎn)旋翼能有效的改善傾轉(zhuǎn)旋翼機懸停和巡航狀態(tài)下的氣動效率,本文提出了變直徑傾轉(zhuǎn)旋翼試驗?zāi)Ｐ驮O(shè)計方案,完成了可變直徑傾轉(zhuǎn)旋翼的結(jié)構(gòu)設(shè)計,并利用虛擬樣機技術(shù)對變直徑傾轉(zhuǎn)旋翼的運動特性、結(jié)構(gòu)動力學(xué)特性以及結(jié)構(gòu)強度進行了分析、研究。