傾轉旋翼,tiltrotor英語短句,例句大全

傾轉旋翼,tiltrotor
1)tiltrotor傾轉旋翼
1.Modeling and analytical investigation on rotor/wing aerodynamic interaction for tiltrotor aircraft;傾轉旋翼機旋翼對機翼氣動干擾的建模及分析
2.Calculated method and parametric effect investigation of wing download of tiltrotor aircraft;傾轉旋翼機機翼向下載荷的計算方法及參數影響分析
3.Experiment on aeroelastic characteristics of tiltrotor aircraft in transition flight;傾轉旋翼/機翼耦合系統過渡狀態氣彈動力學試驗研究

英文短句/例句

1.Calculation of the Aerodynamic Interaction between Rotor／Wing／Fuselage of Tilt-Rotor;傾轉旋翼飛行器旋翼/機翼/機身氣動干擾計算
2.Review of Aeroelastic Stability Investigations for Tiltrotor Aircraft傾轉旋翼機氣動彈性穩定性研究進展
3.Modeling study on tilt-rotor's aeroelastic stability in cruise flight前飛狀態傾轉旋翼機氣彈穩定性建模
4.Bell/Boeing 609--First Civil Tiltrotor貝爾/波音609民用傾轉旋翼飛機——民用飛機的新葩
5.Study on Some Aeroelastic and Stability Analyses of Tiltrotor;傾轉旋翼機氣彈響應及穩定性若干問題研究
6.Design and Realization of the Servo System for Tiltrotor Model Bench;傾轉旋翼模型實驗臺伺服系統設計與實現
7.A Mathematical Model of Tilt-rotor Flight Dynamics and Investigation of Flight Control in Transition Mode;傾轉旋翼飛機過渡模式動力學建模與控制研究
8.Research on Application of the Virtual Prototyping Technology to Tilt-Rotor Design;虛擬樣機技術在傾轉旋翼設計中的應用
9.Research on Tilt Rotor Vertical Take-Off and Landing Roll Channel Control Problem;傾轉旋翼機垂直起降滾動通道控制問題研究
10.Research of Dual Model Reference Adaptive Control System for Tilt-Rotor Aircraft傾轉旋翼機模型參考自適應雙重控制系統研究
11.Design and Research of Control law for TiltRotor in Transition Flight Phase傾轉旋翼機過渡飛行階段控制律設計研究
12.Full Envelope Flight Control Method for Small Unmanned Tilt Rotor Aircraft小型無人傾轉旋翼機全模式飛行操縱控制
13.Design of Flight Control System for a Small Unmanned Tilt Rotor Aircraft小型無人傾轉旋翼機飛行控制系統設計(英文)
14.Computational analysis on tiltrotor aerodynamic characteristics for transitional flight過渡狀態的傾轉旋翼氣動特性計算分析(英文)
15.Control Strategy for Tilt-Rotor Aircraft Trimming in Steady Level Flight傾轉旋翼飛行器的操縱策略和配平方法
16.A Mathematical Model of Unmanned Tiltrotor Aircraft and Research on Attitude Control System Design;無人傾轉旋翼機飛行力學建模與姿態控制技術研究
17.Design of Operation Unit and Its Control System for Tiltrotor Model Bench;傾轉旋翼模型實驗臺的操縱機構及控制系統設計
18.A Method of Stability Evaluation of Tiltrotor in Helicopter Mode傾轉旋翼機直升機狀態系統穩定性判斷的一種方法

相關短句/例句

tilt rotor傾轉旋翼
1.Multidisciplinary design optimization for aerodynamics/structural dynamics of tilt rotor blade;傾轉旋翼槳葉空氣動力學/結構動力學多學科優化設計研究
2.Considering the operational characters of tilt rotor/propeller,a design method for tilt rotor/propeller is presented.針對小型傾轉螺旋槳獨特的工作特性,在研究國外有關傾轉旋翼槳葉設計現狀的基礎上,本文運用了遺傳算法對槳葉的參數進行了尋優設計分析,以滿足不同飛行狀態的性能要求。
3.The new-concept variable diameter tilt rotor (VDTR) which has a combined aerodynamic advantage of a large-diameter rotor in hovering flight and a small-diameter rotor in cruise flight represents a key developmental direction of the tilt rotor.新概念變直徑傾轉旋翼綜合了懸停時大尺寸旋翼和巡航時小尺寸旋翼的氣動優點,是傾轉旋翼飛行器的一個重要發展方向。
3)tilt-rotor傾轉旋翼
1.<Abstrcat> In the present paper, the rotor wake of tilt-rotor aircraft is classified into the steady wake in hover and forward flight and the unsteady wake in transition flight, and a rotor free-wake analytical method for tilt-rotor aircraft has been developed based upon the Weissinger-L lifting-surface theory and rolled-up tip vortex model.將傾轉旋翼機的旋翼尾跡問題區分為二類,即懸停和前飛等狀態的定常尾跡以及過渡飛行狀態的非定常尾跡。
2.In this paper, the aerodynamic interactions between rotor/wing/ fuselage of tilt-rotor in hover and transition flight was calculated.本文計算了傾轉旋翼飛行器懸停狀態和過渡飛行狀態的旋翼/機翼/短翼/機身之間的氣動干擾和氣動特性,分析了其特點,并進行了初步的試驗驗證。
3.This thesis is aimed at the interaction aerodynamics problem on the rotor flowfield of a helicopter and a tilt-rotor aircraft by applying the rotor vortex theory and the panel method, and the major contributions of the author s research work are as follows:Based on the blade Weissinger-L model, rotor roll-up tip vortex model .本文采用渦流理論方法和面元方法，對直升機和傾轉旋翼機的旋翼下洗流場的干擾空氣動力學問題進行了較為深入的研究。
4)tiltrotor傾轉旋翼機
1.The parameter uncertainty in tiltrotor model caused by the variation of nacelle angle was considered in controller designing for flight mode conversion of tiltrotor.針對傾轉旋翼機過渡段模型參數攝動問題,在狀態方程描述的框架下,用線性分式變換形式將模型參數攝動表示為對角塊結構,采用μ綜合方法設計了傾轉旋翼機過渡段飛行控制器。
2.The airplane mode s model of tiltrotor was founded.建立傾轉旋翼機飛機模式的分析模型,分析系統的頻率和阻尼特性,揭示了對系統穩定性起主要作用的一些模態;分析了旋翼擺振運動、機翼氣動力和自轉狀態假設對系統穩定性的影響;分析了系統一些重要參數,如槳葉固有頻率和機翼固有頻率,對系統回轉顫振穩定性的影響。
3.The multi-body analysis of the aeroelastic stability of the tiltrotor aircraft is presented.通過多體動力學方法建立了傾轉旋翼機動力學分析模型。
5)tiltrotor aircraft傾轉旋翼機
1.Dynamic stability analysis of tiltrotor aircraft in forward flight;傾轉旋翼機前飛動力學穩定性分析
2.Considering the characteristics of the thrust vector/aerodynamic force multiple control for tiltrotor aircraft, this paper,based on the model of the tiltrotor aircraft, designs the flight control system using variable structure control with sliding mode.文中針對傾轉旋翼機拉力矢量/氣動力組合控制的特點,在完成傾轉旋翼機建模的基礎上,采用滑模變結構控制對飛行控制系統進行了設計。
3.In this paper the flight control system of tiltrotor aircraft is designed by using linear model following method to resolve the coupling of lateral channel.文中針對傾轉旋翼機橫側向飛行控制系統的耦合問題,應用線性模型跟隨法進行控制器的設計。
6)tilt-rotor傾轉旋翼機
1.Natural characteristic analyse of the transmission of Tilt-Rotor;某型傾轉旋翼機傳動系統固有特性分析
2.Dynamic response analysis of the transmission of tilt-rotor in different modes;傾轉旋翼機傳動系統多狀態響應特性研究
3.Modeling study on tilt-rotor's aeroelastic stability in cruise flight前飛狀態傾轉旋翼機氣彈穩定性建模