low-speed aircraft 中文意思是什麼

low-speed aircraft 解釋
低速飛機
  • low : adj 1 低的；淺的，矮的。 low flight 低飛。 a low temperature 低溫。 low tide [water] 低潮。 The g...
  • speed : n 1 快，迅速。2 速率，速度。3 （汽車的）變速器，排擋。4 （膠片，照相紙）感光速度。5 〈古語〉興隆...
  • aircraft : 飛機（單復數同）
  1. This dissertation presents how to use the ultrasonic motor as an actuator to suppress the flutter of a two - dimensional airfoil section with a control surface. the ultrasonic motor, which features simple structure, high torque at low speed, small size, low weight and no electromagnetic contamination, is a promising actuator for the flutter suppression of small aircraft

    超聲電機以其結構簡單緊湊、轉矩/質量比大、低速大扭矩、直接驅動，動態響應快、斷電自鎖和不產生磁場且不受外界磁場干擾等優點，有望成為一種非常有前途的作動器，用於小型飛機的機翼顫振主動抑制。
  2. With the development of the aircraft performance at low altitude and high speed, as well as the marked progress of eco - environmental protection, the issue of bird impact to aircraft has been concerned more and more

    隨著航空器低空高速性能的發展，以及生態環境保護工程卓有成效的工作，飛行器結構鳥撞問題越來越引起人們的注意。
  3. If the aircraft moves from a high - speed air stream to a low - speed air stream, it may experience a large headwind loss resulting in a sinking motion

    當飛機由高速氣流進入低速氣流時，逆風則會大為減弱，令飛機下沉。
  4. When an aircraft flies at a high speed in the low altitude, bird impact possibly occurs

    飛機在低空、高速飛行時，可能會遇到飛鳥的撞擊。
  5. To study the aircraft - engine stability assessing technology about total - press distortion, four different structure insert - boards and testing schemes are designed, based on the technology of russian insert - board distortion and assessing compressor stability of english and usa. the low speed compressor ( lsc ) at college of energy and power in nuaa is used to carry out the all insert - board distortion experiments studies

    為了能夠更清楚地認識俄羅斯關于總壓畸變下的航空發動機穩定性評定的技術，本文在了解俄羅斯插板畸變試驗技術和英美等國家的穩定性評定技術的基礎上，設計了4塊不同結構形式的插板畸變擾流器裝置及試驗測量方案，利用南京航空航天大學能源與動力學院的低速大尺寸軸流壓氣機（ lsc ）試驗器，完成了各插板的畸變試驗。
  6. In the flight experiment of aircraft, the mass data acquisition, storage and transfer is always one important part of system, especially for the measurement of parameters such as temperature and pressure of cockpit. in order to meet these needs, we design this simultaneous data acquisition system with multi - channel and large - capacity, which is based on single chip microprocessor and usb interface. it overcomes some shortcomings of traditional devices such as : big size, short work time, small memory capacity etc. it also has many advantages of high speed, low power dissipation, ease - of - use, ease to expand port, supporting plug - play, low - cost etc, so it will be used very widely

    在飛機的飛行試驗中，海量數據的採集、存儲和傳輸一直是系統非常重要的一部分，尤其是對飛行員駕駛艙環境控制系統的溫度、壓力等參數的測量來說更是如此。本文根據課題實際需要，研製的基於單片機和usb介面的多通道、大容量、便攜式數據採集系統，克服了現有設備體積大、工作時間短、存儲容量小等缺點。同時，本系統還具有功耗低、速度快、使用方便靈活、易於擴展、支持即插即用、成本低廉等一系列優點，具有廣泛的應用前景。
  7. A stability approach of the whole aircraft low speed flutter model suspended in the wind tunnel analysis

    全機低速顫振模型的全機穩定性分析
  8. Aircraft traversing through alternating high - speed and low - speed air streams may encounter headwind losses and gains at different locations along the approach and departure corridors

    當飛機沿著進場或離場走廊穿越這些高低速交替的氣流時，可能會在不同位置遇到逆風減少和增加的情況。
  9. Lying between these high - speed air streams are air streams of lower wind speed. aircraft traversing through alternating high - speed and low - speed air streams may encounter headwind losses and gains at different locations along the approach and departure corridors

    當飛機沿著進場或離場走廊穿越這些高低速交替的氣流時，可能會在不同位置遇到逆風減少和增加的情況。
  10. Flight simulator plays an important role in hardware - in - loop simulation, and a high - quality simulator is critical in developing a high - performance aircraft. this paper focuses on the performance improvement, it develops the controller of three axises and adjusts the control parameters in frequency - domain. it also concerns about some factors that influence the low - speed performance and draws some conclusions about the key points of performance improvement

    本論文針對轉臺的品質整定，基於頻域法設計與實現了轉臺三軸的控制器，在頻率域內整定了轉臺的動靜態品質，並對整定過程中的問題和現象作了詳細的分析和研究，提出了轉臺品質整定的關鍵點和注意點。
  11. The mechanism of two possible ways of thrust vectoring control : force and moment control are analyzed. the effects of thrust vectoring on aircraft supersonic performance, take - off and landing performance, low speed and high angle of attack performance are studied. the air combat effectiveness of thrust vectoring control and post - stall maneuvers are also analyzed

    5 、分析了推力矢量的兩種應用方式：力控制和力矩控制的機理，研究了推力矢量對飛機超音速性能、起降性能、低速大迎角性能的影響，討論了推力矢量與過失速機動對空戰效能的影響。
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