渦流轉速計 的英文怎麼說

中文拼音 [guōliúzhuǎn]
渦流轉速計 英文
eddy-current tachometer
  • : 渦名詞1. (漩渦) eddy; whirlpool; vortex 2. (酒窩) dimple
  • : Ⅰ動1 (液體移動; 流動) flow 2 (移動不定) drift; move; wander 3 (流傳; 傳播) spread 4 (向壞...
  • : 轉構詞成分。
  • : Ⅰ形容詞(迅速; 快) fast; rapid; quick; speedy Ⅱ名詞1 (速度) speed; velocity 2 (姓氏) a surna...
  • : Ⅰ動詞1 (計算) count; compute; calculate; number 2 (設想; 打算) plan; plot Ⅱ名詞1 (測量或計算...
  • 轉速 : speed; revolution; rotation rate; speed of revolution; rotating speed; rotational speed轉速指示器...
  1. There are five parameters need to be measured. there are five channels for input : the displacement of casting - roller, the rotate speed of casting - roller, the pressure of casting and rolling, the casting temperature and the water - speed of cooling water. they are measured by raster, photoelectric coder, strain pressure sensor, thermocouple and turboflowmeter

    系統需要進行監測的參數有五個,即有五路輸入信號:鑄輥位移、鑄輥、鑄軋壓力、澆鑄溫度、冷卻水,分別採用光柵、光電編碼器、應變式壓力傳感器、熱電偶和作為檢測元件。
  2. With this axial symmetric quasi - 3d model, the gas - flow field in such a wedge - shape air - gap is studied, the phenomena about taylor vortex in such a narrow wedge - shape air - gap is illuminated and the so caused gas - flow in axial direction is explained

    採用準三維軸對稱的算模型,對楔形氣隙的場進行了研究,驗證了高情況下,環形間隙場中充滿taylor的現象及相關規律。
  3. Nasa - 37 transonic and nwpu - 1 subsonic rotors are calculated by using this program. results of calculation indicates that this program can admirably simulate rotor rows flow in axial compressors and distinguish passage shock, leakage vortex path and separation of boundary layer

    用該程序分別算了nasa - 37跨音子和nwpu - 1亞音子,算結果表明本文建立的孤立子程序能夠較好的模擬軸壓氣機葉片排內動情況,能夠有效的捕捉通道激波和間隙泄漏軌跡以及葉片附面層的分離。
  4. The principal contributions of this dissertation are : 1. a high fidelity and real - time rotor wake inflow model was built up. based on peters - he finite states wake theory, a new influence coefficient matrix for high speed flight was derived, the modified wake model is better suitable for the flight state with a large wake skew angle

    本模型以peters - he有限狀態尾跡理論為基礎,修正了大尾跡傾斜角時的誘導度影響系數矩陣,並結合了王氏理論,導出了旋翼誘導度垂向分量和旋分量的表達式,可算平尾、尾槳和垂尾氣動中心處誘導度各分量。
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