風洞實驗室 的英文怎麼說

中文拼音 [fēngdòngshíyànshì]
風洞實驗室 英文
wind tunnel laboratory
  • : 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
  • : Ⅰ形容詞1 (內部完全填滿 沒有空隙) solid 2 (真實; 實在) true; real; honest Ⅱ名詞1 (實際; 事實...
  • : 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
  1. With development of high - speed missile imaging detection aero - optical effects, certain accomplishments on theoretical analysis have been obtained. the laboratory test system needs to be built to vertify the correctness and validity of theory. at the same time, to study the transient influence of high - speed flow on image transmission, an aero - optical effect experiment of wind tunnel is needed furtherly on the foundation of the transform of wind tunnel, in order to use the researching accomplishment of aero - optical effects in the aero - optical distortion image adjustment evaluation

    隨著高速導彈成像探測氣動光學效應機理研究工作的深入開展,在理論分析上取得了一定的成果,需要搭建系統來證理論的正確性和有效性,同時為了較真地研究高速流場對圖像傳輸的瞬態影響效應,需要在改造的基礎上進一步進行氣動光學效應,期望將獲得的氣動光學效應研究工作成果用於氣動光學畸變圖像校正效果的評估。
  2. Pedestrian level wind concerns are also addressed, in this paper, the wind pressure distribution on the surface of yingli building in chongqing is introduced. a wind tunnel test of yingli building rigid model is investigated in beijing university environment wind tunnel laboratory

    並以興建於重慶市的重慶英利大廈為對象,在北京大學環境學院環境風洞實驗室進行,系統地研究了該建築外表面平均壓分佈和脈動壓分佈特性,給出了可用於設計的荷載值,以確保大樓的安全性與穩定性。
  3. 2. the model experiment aimed at the aerodynamic effect of large high - speed landslides has been accomplished in wind tunnel laboratory for the first time. on the base of testing research, the paper studies different factor which influence the aerodynaxnic effect of flying 1andslide, and numerically simulates the aerodynamic effect with the help of the hydrodynamics finite element

    ( 2 )首次在風洞實驗室進行了針對大型高速滑坡凌空飛行階段空氣動力學效應的模型,研究了影響飛行滑坡巖體空氣動力學效應的不同因素;應用流體力學有限單元法對飛行滑坡巖體的空氣動力學效應進行了數值模擬。
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