靜子葉片 的英文怎麼說

中文拼音 [jìngzipiān]
靜子葉片 英文
stationary blade
  • : Ⅰ形容詞1. (安定不動; 平靜) still; calm; motionless 2. (沒有聲響; 清靜) silent; quiet Ⅱ名詞(姓氏) a surname
  • : 子Ⅰ名詞1 (兒子) son 2 (人的通稱) person 3 (古代特指有學問的男人) ancient title of respect f...
  • : 片構詞成分。
  1. Abstract : the main features, the key points of design, material selection and test method of international metal and ceramic hybrid type multilayer stator vane are reviewed in this paper

    文摘:評述了國外金屬和陶瓷多層混合式靜子葉片的主要特點、設計要點、材料選擇和試驗方法。
  2. By using harika algorithm, the characteristic of a high - pressure compressor is calculated at different installation angle of the inlet guide vane and the stator vanes ; the characteristics of a high - pressure turbine and a low - pressure turbine are simulated at different installation angles of the guide vane based on ainley method

    本文用harika演算法計算了導流靜子葉片安裝角度可調的變幾何高壓壓氣機特性;用ainley法計算了渦輪導向器面積可調的高壓渦輪和低壓渦輪的特性。
  3. In order to investigate the unsteady flow frequency domain performances of an axial flow compressor at different mass flow, rotating speed and blade row spacing, plus inlet flow distortion, and considering aerodynamic characteristics and stability of the compressor, the low speed research compressor ( lsc ) at college of energy and power in nuaa is used to carry out the experiment studies. a large amount of test data has been gained through dynamic pressure transducers embedded in the stator blades at the tip, middle and hub section, then fast fourier transform algorithm ( fft ) is applied to calculate the frequency data

    為探討軸流壓氣機在工作流量、工作轉速及動?排軸向間距變化時的排流場非定常頻譜特性變化規律,並耦合進氣畸變的影響,同時與壓氣機氣動性能和氣動穩定性相關聯,作者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,採取在靜子葉片表面埋入動態壓力傳感器的實驗方法,對尖、中和根三個截面的動態壓力進行了測量,獲得了大量的可靠的實驗數據。
  4. One " golden dragon " fruit is set behind another one that is shown cut into halves, displaying two similar circles close together. several leaves, green but warm, lie peacefully in a wicker basket

    一個切成兩半的金果,並列著兩個同樣的圖形一個完整的金果置於其後,還有幾溫暖的綠色,一起安地在帶有細細提手的竹籃內休息。
  5. The propose of this project is to develop a three - dimensional, compressible navier - stokes solver for detailed study the flow inside transonic turbine and compressor ' s stator in the airplane turbomachinery

    摘要本研究的目的在發展一系列飛機滑輪引擎之靜子葉片的計算流體力學方法與程式,計算程式方面包括三維格點的建立與黏性流程式開發及撰寫等,程式發展完成後將進行一系列外形及氣流條件計算模擬。
  6. The compressor exists about 0. 265 rotor blade converted frequency near stall point, its intensity increases with rising of rotating speed and reducing blade row spacing. the blade row spacing would exert influences on rotor - stator interaction, stability and stall mode

    在臨近失速點處,不同工作轉速、不同動?排軸向間距均存在約為0 . 265轉摺合頻率的特徵頻率擾動,強度隨轉速的上升和軸向間距的減少而增大。
  7. This paper uses the theory of design on parameters to achieve the software package of bss and the stator vane ’ s vibration and fatigue analysis software, which realize the process of stator vane ’ s vibration and fatigue use a key to control

    本文還採用了參數化的設計思想開發了盲源分離的軟體包。同時課題期間還開發了靜子葉片振動與疲勞分析平臺軟體,實現了整個振動、疲勞特性分析的過程的「一鍵控制」 。
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