熱風洞試驗 的英文怎麼說

中文拼音 [fēngdòngshìyàn]
熱風洞試驗 英文
hot tunnel climatic test
  • : Ⅰ名詞1 (空氣流動) wind 2 (風氣; 風俗) practice; atmosphere; custom 3 (景象) scene; view 4 ...
  • : Ⅰ名詞(物體上穿通的或凹入較深的部分; 窟窿; 洞穴) hole; cavity Ⅱ形容詞(深遠; 透徹) profound; thorough; clear
  • : 名詞(古代占卜用的器具) astrolabe
  • : 動詞1. (察看; 查考) examine; check; test 2. (產生預期的效果) prove effective; produce the expected result
  • 風洞 : [航空] wind tunnel; air tunnel; whirl tube; wind tunnel plant; flume
  • 試驗 : trial; experiment; test
  1. The tests were conducted in the hypersonic low density wind tunnel at nominal test conditions of mach 16, stagnation temperature 923k, stagnation pressure 1. 40mpa and 7. 30mpa. heat - transfer data were obtained on a hemisphere model, a sharp cone and a big blunt cone respectively by means of infrared thermal mapping techniques, that of a 0. 5mm thickness blunt cone by virtues of thermocouples. furth ermore, heat - transfer on all those models was calculated with the theoretical method

    最後在名義m _ = 16 、 t _ 0 = 923k 、 p _ 0 = 1 . 40mpa及7 . 30mpa的高超聲速低密度中,利用紅外圖技術獲得了半球圓柱、尖錐、大鈍頭三個模型表面流分佈,利用薄壁法技術得到了一壁厚為0 . 5mm的鈍錐模型表面的流分佈,並通過工程理論方法計算了模型表面的氣動,把理論計算結果與上述結果比較,幾者符合得較好。
  2. The optimized heat exchangers module was verified to be good based on wind tunnel test and road test

    改進方案的和實車路結果表明,各散器的散量達到設計指標,各系統工作正常。
  3. The demonstration of heat - transfer measuring techniques and prospect of infrared thermal mapping techniques, main parts and performance indexes of a infrared camera, functional blocks and implementation of infrared processing software, experimental facility and measuring system of the wind tunnel has been made. the model emittance was experimentally determined and the three methods correcting directional emittance were compared. those problems of the infinite - slab model thickness and constant wall heat rates hypothesis, the determination of adiabatic wall temperature were discussed in a 1 - d heat conduction analysis

    本文對紅外圖測技術與應用前景、紅外像儀主要部件與性能指標、紅外測數據處理軟體功能模塊與實現、設備與測量系統等進行了論述,測量了模型表面發射率並對發射率隨極角變化的三種修正方法進行了對比,對一維傳導分析中模型壁厚半無限假設、壁面流定常假設、絕壁溫選取等進行了探討。
  4. The static pressure distributions of turbine blade surface were measured under five different circumstances and heat flux distributions of turbine blade were measured under two different circumstances. the experiment ' s accuracy, reliability were discussed

    對激波管臺的測精度、可靠性進行討論表明該種實方式對渦輪流場測壓、測具有令人滿意的精度。
  5. The latter, which had such these virtues as non - contact measurements, small flow field disturbances and larger measured areas, was widely applied in wind tunnel tests

    紅外圖技術是一種非接觸測量技術,具有對流場無干擾、大面積測量等優點,在中獲得了廣泛的應用。
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