飛翼飛機 的英文怎麼說
中文拼音 [fēiyìfēijī]
飛翼飛機
英文
aircraft; all-wing-
In order to improve the capability of asw, navy has, preliminarily been equipped with modern anti - submarine weapons, among which helcopter serves as the core. consequently, for the formation of the powerful combat capability, there is an urgent need of building an airborne anti - submarine tactical data system ( tds ), which carries out comprehensive information processing and fulfils inflight commanding and guiding
為了提高我軍的航空反潛水平,我軍已初步具備以旋翼飛機為核心裝備的硬體航空反潛能力,急需構建適應我軍現役搜、攻潛武器裝備的機載反潛戰術數據系統( tds ) ,使我海軍在航空反潛方面形成強大的戰鬥力。It ' s the count, in his autogiro
那是伯爵,駕駛著他的旋翼飛機Backswept wing aircraft
后掠翼飛機It dates from 125 million years before biplanes were invented
在雙翼飛機問世之前的1 . 25億年前,這種動物翱翔在天空。In 1919 a vickers vimy biplane won the great london - to - australia air derby. seventy - five years later pilots matched the feat in this vimy replica
1919年,維克斯公司生產的維美號雙翼飛機贏取了倫敦? ?澳洲飛行大賽。七十五年以後,飛行員用維美好的復製品重新表演了精彩的飛行演出。Buzzing aussie isles, pilots peter mcmillan and lang kidby are in the home stretch of their england - to - australia flight in a replica vickers vimy biplane
飛行員彼得?麥克米蘭和讓?基德比乘坐著維基維美號雙翼飛機的復製品正掠過澳洲境內的小島,這里離他們的家鄉,英格蘭? ?澳洲飛行的終點已經越來越近。Joined - wing configuration features diamond - shapes in both the plan and front views. the front wing is aft swept with positive - dihedral angle and the rear wing is forward swept with negative dihedral angle
聯結翼飛機是指帶上反角的后掠前翼和帶下反角的前掠后翼聯結成菱形框架結構的飛機。The first such machine, a radio - controlled “ fairey queen ” biplane, was catapulted into the air in 1933 and survived two hours of live fire from a british warship
首架這樣的飛行機是一架由無線電控制的雙翼飛機,且名為「仙境中的女王」 , 1933年被彈射而飛向天空,並在一艘英國軍艦的炮轟下挺了兩個小時。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。With additional capabilities in rotorcraft, electronic and defense systems, missiles, rocket engines, satellites, launch vehicles and advanced information and communication systems, the company ' s reach extends to customers in 145 countries
加上旋翼飛機、電子和防禦系統、導彈、火箭發動機、衛星、運載火箭和先進信息及通訊系統等方面的研製能力,本公司的客戶已經遍及145個國家。The effects of body - strake on lift characteristics of the double - delta - wing aircraft
機身邊條對雙三角翼飛機升力特性的影響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,適合於飛行包線內的所有模式,為傾轉旋翼飛機飛行動力學的進一步研究提供了基礎。Tilt - rotor aircraft combine the vertical takeoff and landing ( vtol ) capability of helicopters with the high speed performance of turboprop airplanes. located at the tips of the wing, the prop - rotors act as helicopter rotors when flying vertically and as airplane propellers in cruising flight
傾轉旋翼飛機翼尖安裝可以傾轉的發動機短艙和旋翼系統,可以在飛行中根據需要在固定翼模式和直升機模式之間轉換,充分發揮直升機垂直起降、懸停及固定翼飛機高速巡航的優點。Structural modeling and aeroelastic analysis of high - aspect - ratio composite wings
飛翼飛機穩定性與操縱性研究Helicopters from a carrier could provide support to potential amphibious operations ; fixed - wing aircraft operating from a carrier could provide greater air defense over a potential beachhead
承運人可以提供直升機支援兩棲作戰潛力;固定翼飛機從承運人可以提供更大的防空超過潛在灘頭But fcs and " fly / fire " coupler is the key technique of iffc 。 in this paper, a fire control system of armed helicopters for ground attack is proposed based on the attack system of fix - wing. we stress on our research of fcs, iffc and " fly / fire " coupler for armed helicopters
本文在參考固定翼飛機攻擊系統的基礎上,建立武裝直升機對地攻擊的火控系統,重點對直升機飛行控制系統、綜合飛行/火力控制系統、以及飛行/火力耦合器等進行了研究。Furthermore, because rotors are mounted on the tips of the wing, the rotor / pylon / wing aerodynamic interactions are also included in the model. such factors reflect the unsteady and nonlinear characteristics in the model
此外,傾轉旋翼飛機的旋翼安裝在翼尖,旋翼/發動機短艙/機翼之間的氣動干擾是建模的一個難點。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A variable control surface on the trailing edge of an aircraft wing, used primarily to increase lift or drag
襟翼飛機后翼上最初用來增加上升力或拖力的可靈活控制的輔助翼分享友人