起飛角 的英文怎麼說

中文拼音 [qǐfēijiǎo]
起飛角 英文
angle of departure
  • 起 : 起Ⅰ動詞1 （站起; 坐起） rise; get up; stand up 2 （取出; 取走） draw out; remove; extract; pull 3...
  • 飛 : Ⅰ動詞1 （鳥、蟲等在空中活動） fly; flit 2 （利用動力機械在空中行動） fly 3 （在空中飄浮遊動） fly...
  • 角 : 角Ⅰ名詞1 （牛、羊、 鹿等頭上長出的堅硬的東西） horn 2 （古時軍中吹的樂器） bugle; horn 3 （形狀像...
  • 起飛 : （of aircraft） take off; lift-off; launch; hop off
  1. The delta-winged columbia, before reaching the orbit, jettisoned its dual booster rockets two minutes into flight.

    三角翼的哥倫比亞號航天飛機在進入軌道前，起飛兩分鐘就拋下其兩個助推火箭。
  2. The calculation results indicate that the starting performance of forebody / inlet with wedge - shaped lip is better than that with plane lip at low flight mach number. at high flight mach number, the performance of the forebody / inlets designed by the two methods is approximate. at low flight mach number, the starting performance of forebody / inlet designed by the method of constant shock wave intensity is better

    結果表明：唇口帶楔角的進氣道在低飛行馬赫數下的起動性能優于唇口平直的進氣道；採用等激波強度和等激波角度方法設計的進氣道在高飛行馬赫數下的性能相近，在低飛行馬赫數下，採用等激波強度方法設計的進氣道起動性能較優。
  3. And her head jerked in spasms, making a spattering noise ; her antennae crisped and burnt away and her heaving mouthparts cracked like pistol fire

    她的頭一陣痙攣，發出飛濺聲，她的觸角變皺然後燒沒了，然後她翹起的口器像手槍開火那樣破裂。
  4. The unique spaceship climbed straight into the blue sky after a thunderous lift-off from cape canaveral.

    這艘獨特的宇宙飛船在轟鳴聲中從卡納維拉爾角起飛了，直沖藍天。
  5. One ornithologist had devised a formula to compute the ratio of domestic to pure - strain wild turkey in an individual bird by comparing the angle of flight at takeoff and the rate of acceleration

    有個鳥類學家設計了一種計算公式，對家養火雞和純種野火雞進行起飛角度和加速度的比較。
  6. Designing idea : when the wind blow, dandelion begin their adventure. they embracing the blue sky, run after the rainbow, apan the flowery, cast about for everywhere of the world, then arrive at a place full of dreams waiting for a brighter future

    設計構思：清風一起，漫天飛舞的蒲公英開始了他們的冒險，他擁抱藍天、追逐彩虹、跨越山川、越盡花林，尋遍世界的每一個角落，然後，棲息到那個充滿夢想的地方，等待著新的明天
  7. On january 28th, 1986, the space shuttle " challenger " exploded 73 seconds after liftoff from cape canaveral, killing all seven crew members

    1986年，挑戰者太空梭于開納非羅角起飛后73秒爆炸，機上七位成員全部罹難。
  8. Then they fell silent, and drifted away upon their dream wings to the far regions of the earth to invite all the crowned heads and their families and provide gratis transportation to them

    他們又陷入沉默，幻想的翅膀飄然而起，飛向全球的各個角落，邀請所有的王公貴族和他們的家人，並且白送他們路費。
  9. Second, by computing the trajectory of the missile and the method of analyzing cep, influences that the fighter ' s height, speed, pitch angle, the deflection angle between fighter and target, and the target moving characters make on the times of fighter attack and missile launch are deeply developed. third, by relating the motion of the missile and the fighter, the influences that fighter ' s dive angle and the deflection angle between fighter and target make on the attack field of the fighter are discussed in this paper when the fighter perform vertical and horizontal attack. criterion of attack effect is proposed focusing on attack time of the fighter, trajectory of the missile and destruction probability to the target

    本文主要完成了以下幾個方面的工作：對導彈可發射區和飛機可攻擊區進行建模，通過對導彈彈道的模擬計算，並運用典型的圓概率偏差精度分析方法，詳細討論了飛機實施攻擊時，飛機的飛行高度h 、速度v 、俯仰角、與目標的偏離角_ x及目標運動特性等對飛機攻擊時機和導彈發射時機的影響；因此，將飛機和導彈結合起來，詳細研究了飛機在垂直平面和水平平面內實施攻擊時，飛機俯沖角和與目標的偏離角_ x對飛機的攻擊范圍的影響；以飛機實施攻擊的時間t 、彈道特性和對目標的殺傷概率p來評判對地攻擊的效果；最後給出典型算例，通過對空地攻擊過程的模擬實現，對飛機飛行過載提出要求。
  10. The position and size of the monochromator, focusing curvature radii and tilting angles of the germanium focusing monochromator under different different take - off angle, size and divergency of the second collimator and intensity loss due to the use of it were determined. the neutron flux at different wavelength, under different reflection and take - off angle of the monochromator and divergency of the first collimator, were given. the simulation on the aperture used for limiting beam size in front of the sample showed that, smaller the size of the aperture and further the distance from the aperture to the sample, greater the loss of the intensity and more serious the spread of the beam along vertical direction at the sample position which makes the practical sampling volume greater than expected

    用蒙特卡羅模擬方法對中子應力衍射譜儀的設計方案進行了優化研究，提出了一系列可供參考的數據：確定了單色器的位置、尺寸、垂直聚焦單色器在不同起飛角下的聚焦曲率半徑和傾角；討論了第二準直器的尺寸和發散，以及使用第二準直器造成的強度損失；給出了在不同單色器反射面、起飛角、中子波長和第一準直器發散度的情況下樣品處的中子注量率，以及多種組合情況下譜儀的解析度曲線；對限束方孔的尺寸、距離樣品遠近對強度損失和測量中的影響做了深入研究。
  11. According to purpose of the towed flight, a new trajectory consisting of taking off, climbing phase, level flight phase is presented with. trajectory pitch angle of the towing plane is optimized. according to the flight law of the towing plane, the fin deflection angle and amplification coefficient of particle - system trajectory of carrier rocket are designed, in order to realizing flight steadily of the carrier rocker

    根據牽引飛行的目的，對載機應用了「起飛?爬升?平飛」的變軌道飛行方案，同時對載機軌道的傾角、傾角變化規律進行優選設計；再根據載機的飛行規律，對運載器質點系軌道的舵偏規律及其放大系數進行了設計計算，實現運載器穩定牽引飛行。
  12. In the story “ the peacock flies southeast ” for example, the main character, jiao chung - ching, and his wife, liu lan - chi, are very much in love

    譬如孔雀東南飛的故事中，男主角焦仲卿跟他太太劉蘭芝感情非常好，但是焦仲卿的母親非常看不起她的媳婦，因此找了各種理由要把這個媳婦給逼走。
  13. As for stamp products, they are unique derivatives of postal service. they get to travel, and sometimes the journeys will take them cross the oceans to far - off lands where they are perceived as emblems of the issuers

    郵票向來都是郵政服務的獨有產品，每一枚郵票都有機會飛越重洋，走進世界每一個角落，肩負起發行地形象大使的責任。
  14. Then in allusion to biased momentum wheel system, based on classical control system a pid controller was design about pitching channel. according to specialty of roll - yawing channel, this paper discuss long - time cycle movement and short - time cycle movement. when design the control method of long - time cycle movement, whiff thruster is used to assistant the control system. when design the control method of short - time cycle movemen, in order to sovle the problem of coundn ’ t abtain the angular velocity signal, nonminimum phase controller advanced by terasaki is used

    然後針對偏置動量飛輪系統，基於經典控制理論設計俯仰通道的pid控制律，根據滾動?偏航通道耦合的特點，分別討論了由軌道角頻率和章動頻率引起的長周期運動和短周期運動。其中長周期運動控制律設計時，結合了噴氣推力控制來輔助偏置動量控制;短周期運動控制中，為了解決不能獲得角速度信號的問題，採用terasaki提出的非最小相位控制器進行控制。
  15. Based on the relationship between the change of the cornea thickness and optical path length, the ablation profile for the correction of wavefront aberration is presented and simulated on computer. the process of scanning - spot excimer laser is studied and simulated on computer. models for calculation of residual wavefront aberration on situations of lateral decentration and torsional misalignment are brought up

    使用改變光程的方法建立起波前像差與角膜切削量之間的關系，並對像差矯正模型進行計算模擬;深入研究了小光斑準分子激光飛點掃描模型，對飛點掃描過程進行計算模擬;提出了中心偏移和旋轉情況下剩餘像差計算模型，為定量研究切削中心定位精度對像差矯正的影響提供了依據。
  16. Arrive 2 hours before flight departure at the skypier to process the check - in procedures check if your onward flight is one of the participating airlines

    從珠三角轉機旅客須于航機起飛前兩小時，抵達海天客運碼頭辦理航空公司旅客登記手續。
  17. This attitude helps to generate greater lift and reduce the distance needed for takeoff or landing

    合適的大迎角，有利於在較低的速度下產生足夠的升力，以便於減少起飛滑跑距離。
  18. When the wind is from the east or northeast, aircraft will depart from hkia towards the northeast until it reaches ma wan where, depending on flight destinations, it may turn south over west lamma channel, or proceed to the southeast passing over tsing yi, the southern part of kowloon peninsula ( such as tsim sha tsui and hung hom ) and the northern part of hong kong island ( such as north point, shaukeiwan and chai wan )

    當吹東或東北風時，飛機向東北方向起飛到馬灣上空時，視乎航班的目的地，飛機可轉向南經西博寮海峽離港，或向東南方向飛越青衣、九龍半島（尖沙咀、紅? ）及港島北部（北角、筲箕灣及柴灣）上空。
  19. Departing flights were climbing at very steep angles, 9. 6 deg for the one shown above. as a result, the aircraft transit the low level jet very close to the end of the runway and the change in head wind was very rapid

    起飛的航機以非常陡的角度爬升，以上提及的飛機用9 . 6度，因此飛機在接近跑道末端經過低空急流而所感受到的逆風轉變非常快。
  20. Spacecrafts are working in the space environment, which is full of sorts of physical mediums. and these mediums will impact on the altitude movement of spacecraft. spacecraft attitude control during propulsive maneuvers is complicated due to several factors as listed below : ( i ) nonlinear dynamics with time delays, ( ii ) modeling and parameter uncertainties, ( iii ) flexible modes due to fuel sloshing and appendages, ( vi ) constraints on propulsive force and torque inputs, ( v ) constraints on acceptable angular rates and attitude, ( iv ) autonomous reconfiguration requirements under failure conditions

    飛行器是在一定的空間環境中飛行，而空間環境中充滿著各種物理介質，對飛行器的姿態運動產生不同程度的影響，所以空間飛行器的姿態控制相當復雜，它受到如下因素的制約： （ ? ）帶時延的非線性動態特性（ ? ）模型和參數的不確定性（ ? ）燃料的激蕩性以及燃料消耗所引起飛行器的質量變化（ ? ）推力和輸入力矩的約束性（ ? ）額定角速度約束和姿態約束（ ? ）在故障發生的情況下自動重新配置的必要性。
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