飛機翼布 的英文怎麼說
中文拼音 [fēijīyìbù]
飛機翼布
英文
aeroplane fabric-
Double - wing micro air vehicles adopts the aerodynamic shape : no tail, only wings and vertical tail placing in wing
雙翼式微型飛行器採用無尾式,且只有機翼,垂尾也置於機翼上的氣動布局。Palmdale, california, 1977, streams of light trace a lockheed tristar landing on automatic pilot. from the cockpit dale activated two cameras mounted on the aircraft ' s vertical stabilizer
美國加利福尼亞,棕櫚谷, 1977年,布魯斯?戴爾,光的流線追蹤著一架靠自動導航降落的洛克希德三星噴氣飛機。戴爾坐在駕駛艙中啟動在垂直穩定翼上的2架相機的快門。Bruce dale, palmdale, california, 1977, streams of light trace a lockheed tristar landing on automatic pilot. from the cockpit dale activated two cameras mounted on the aircraft ' s vertical stabilizer
美國加利福尼亞,棕櫚谷, 1977年,布魯斯?戴爾,光的流線追蹤著一架靠自動導航降落的洛克希德三星噴氣飛機。戴爾坐在駕駛艙中啟動在垂直穩定翼上的2架相機的快門。Salt water corroded the light alloy frames and the fabric wing-covering.
鹽水對輕合金飛機構架和布質機翼蒙皮有腐蝕作用。1909 louis bleriot flew his monoplane across the english channel, in 36. 5 minutes
路易斯?布萊里奧駕駛他的單翼飛機飛越英吉利海峽花了36 . 5分鐘。None of the other p1 - lots present would have thought of going up, but hamel one of the finest of all pilots of the beriot monoplane was not to be stopped
其他在場的飛行員都沒有想到要起飛,但是哈梅爾? ?這個布雷里奧式單翼飛機最優秀的駕駛員之? ? ?是不會被阻攔的。Although aircraft designers and engineers continued to employ wing - warping techniques for years afterward ( especially on early monoplanes such as the bleriot xi ), ever faster flight speeds eventually led them to beef up wing structures to resist the resulting stresses
雖然其後許多年間,飛機設計師和工程師仍繼續採用翹曲機翼設計(尤其是布雷修xi型等早期單翼機) ,但由於飛行速度不斷提升,終于迫使他們加強機翼結構,以承擔所增加的應力。Investigation on application of gurney flap to triplane configuration aircraft lift - enhancement
襟翼增升技術在三翼面布局飛機模型上應用的實驗研究In this paper, the major subject investigated is the ducted fan vertical take - off and landing ( vtol ) uav. compared with normal fixed - wing uav, it has so many strong points such as be convenient to take - off and land, good adaptability and long hover time. we analyze and summary information of foreign uavs, then calculate the figure dimension of our uav, and draw the uav structure configuration and the outside view drawing of three dimensional structure
本課題的研究對象是涵道風扇式垂直起落無人機,與一般的固定翼無人機相比,它有著起落方便、適應性強、可以在空中長時間盤旋等優點,本文通過對相關飛行器資料的分析總結,給出了無人機的大體結構尺寸,並畫出了無人機的結構布局圖和三維結構外觀圖。To study the influence of this damper configuration to aeromechanical stability, some work has been done in this thesis. first, dynamic equation of the rotor - hub system was modeled with the generalized hamilton principle, which can be used to analyze the stability problem in different conditions like on - ground, hovering and flight. when fastening the fuselage, the model can also be used to analyze the stability problem of isolated rotor system
為了研究這種新型布置減擺器對直升機穩定性的影響,本文所作研究工作如下:首先,本文利用廣義的hamilton原理建立了適用於不同狀態(地面、懸停和前飛)的旋翼/機體耦合系統的動力學模型,該模型中將機體固定可以用來分析孤立旋翼的穩定性問題。Design of innovative control surfaces of flying wing aircrafts with large ratio aspect
大展弦比飛翼布局飛機新型操縱面設計Bruce dale, palmdale, california, 1977, streams of light trace a lockheed tristar l * * * ing on automatic pilot. from the cockpit dale activated two cameras mounted on the aircraft ' s vertical stabilizer
美國加利福尼亞,棕櫚谷, 1977年,布魯斯?戴爾,光的流線追蹤著一架靠自動導航降落的洛克希德三星噴氣飛機。戴爾坐在駕駛艙中啟動在垂直穩定翼上的2架相機的快門。Compared with a delta wing aircraft, the double - delta wing configuration has better aerodynamic performance at high angles of attack. an operational analysis was introduced as a method for evaluating training effectiveness of trainer aircraft. approaches to the engineering estimation of aerodynamic characteristics for aircraft with a double - delta wing configuration were studied, and the procedures for determining aircraft performance indices formulated. taking training effectiveness as the objective function and geometric parameters of the wing platform as design variables, through a numerical multivariate optimization arithmetic, the conceptual design optimization for a certain fighter trainer aircraft with double - delta wing configuration was carried out under the constraints of tactical and technical requirements and interrelated geometry. agreement of a calculation example with engineering practice indicates that the optimal design has higher training effectiveness than the baseline design, and in addition, improves the structural force - bearing conditions
雙三角翼氣動布局比三角翼飛機具有更好的大攻角空氣動力特性.引入了評估教練機訓練效能的作戰分析法,研究了雙三角機翼布局飛機空氣動力特性的工程計算途徑以及飛機性能指標的確定方法.以訓練效能作為目標函數並選取機翼平面形狀的幾何參數為設計變量,採用多變量數值尋優方法,在戰術技術指標及相關幾何約束條件下,對某高級教練機的雙三角機翼氣動布局方案進行了優化選擇.算例表明最優方案不僅比原準方案具有更高的訓練效能,還改善了結構的受力情況,與工程實踐吻合During the procedure, the airspeed continues accelerating ( or decreasing ) and the aircraft configuration is rapidly changing. the aerodynamic interactions are complex and lead to dynamic instabilities. the shift between helicopter and airplane flight modes necessitates a change in control strategy
過渡模式下,飛機速度不斷增加(或減小) ,氣動布局不斷改變,飛機動力穩定性差且氣動干擾嚴重,直升機控制和固定翼控制切換,因此過渡模式動力學特性和控制系統研究是整個傾轉旋翼飛機研製的主要難點。This paper explored the micro pressure sensor that is used for the measurement of distributed pressure at the surface of smart - skin. firstly, established the surface pressure model according to the aerodynamic properties, defined the optical measurement system that based on intensity modulation principle, discussed the components of this system and theoretical analyzed its measurement theory in detail
首先,根據空氣流動的基本規律給出機翼表面壓力分布圖,通過對光學式微型壓力傳感器的理論分析,採用強度調製法測量飛機機翼表面的壓力並建立基於此方法的光學測量系統模型,得到了壓力與敏感膜片變形以及光電轉換輸出能量之間的關系。The wings for the aircraft are being built at broughton in north wales, and then transported by sea for final assembly at toulouse in france, using a specially - constructed roll - on roll - off ferry built in shanghai
目前飛機的機翼正在北威爾士的布勞頓進行建造,然後將通過由上海特製的滾裝船海運至法國的圖盧茲進行最後組裝。Structural stiffness effect of single amp; amp; bi - fuselage uav with higher aspect ratio and straight wing
大展弦比直機翼雙機身飛機中機身與機翼的最佳布置問題With it s old name as : shandong xinda trading co., ltd., was established in 1998, specialized in the issuing and making of areoboat, remote controllable umbrella, remote controllable tri - angle wing, motivated hot air balloon, large scale advertising plan and undertake the photo making by air
原名山東省信達商貿有限公司,成立於1998年,專業從事飛艇遙控動力傘遙控三角翼,動力熱氣球大型廣告飛機等空中飛行廣告的發布與製作,並承攬空中航拍業務。分享友人