降低的傾點 的英文怎麼說

中文拼音 [jiàngdeqīngdiǎn]
降低的傾點 英文
depressed pour point
  • : 降動詞1. (投降) surrender; capitulate 2. (降伏) subdue; vanquish; tame
  • : 4次方是 The fourth power of 2 is direction
  • : Ⅰ名詞1 (液體的小滴) drop (of liquid) 2 (細小的痕跡) spot; dot; speck 3 (漢字的筆畫「、」)...
  • 降低 : reduce; cut down; abate; debase; drop; lower; lessening; reducing; reduction; depression; tarnish
  1. Because at present pay of worker of this city company expends scale, be 5 %, the certain proportion that because this needs to press individual capture from inside business pay cost, expends base delimits individual account, the enterprise delimited individual account part is 1998 6 %, will expend as individual capture henceforth proportional rise, the enterprise delimits collapse of individual account share is decrescent little namely scale of individual pay fee increased difficulty 1999 a percent, the enterprise delimits the part reduces a percent, scale of final pay fee rises 8 %, the enterprise delimits the share drops to 3 %

    由於目前本市企業職工繳費比例為5 % ,因此需要從企業繳費中按個人繳費基數一定比例劃入個人帳戶, 1998年企業劃入個人帳戶部分為6 % ,今後隨著個人繳費比例提高,企業劃入個人帳戶部分漸減少即1999年個人繳費比例提高難度1個百分,企業劃入部分1個百分,最終繳費比例提高到8 % ,企業劃入部分至3 % 。
  2. The thermal visualizations of jet impingement cooling with single or double row holes inside semi - enclosed channel are measured by using infrared camera and then the impingement cooling heat transfer coefficients are deduced. the effects of flow and geometry parameters on convective heat coefficients are obtained. the results show that : for a single row normal impingement, the impingement cooling effectiveness is enhanced with the increase of impinging reynolds number or the decrease of hole space to diameter ratio, and the best effectiveness is achieved under the jet - to - surface spacing equals to 2 ; when the jet is oblique to the confined wall, the cooling effectiveness is weaken especially under the jet - to - surface spacing ratio is greater than 2 ; for double rows normal impingement cooling, the cooling effectiveness of rear row jet is weaker than the front row under lower impinging reynolds number or bigger jet - to - surface spacing

    對于單排垂直射流,沖擊冷卻效果隨射流雷諾數增加、孔間距與直徑比減小而得到提高,沖擊間距比為2時換熱效果最好;沖擊孔中心線向通道封閉一側斜后,射流沖擊冷卻范圍變窄,當沖擊間距比大於2時駐對流換熱能力明顯;對于雙排沖擊射流,孔排間距與直徑比增加使沖擊冷卻范圍變大,但在兩排孔之間區域對流換熱系數有所下;在較小沖擊射流雷諾數和較大沖擊間距比下,後排射流沖擊換熱效果要遜於前排射流。
  3. A new aerodynamic design system developed by authors for draft fan with enhanced efficiency, suppressed noise, enlarged flux and high load. the new design system features : a twist regulation for vortex control is employed in designing to lessen the secondary flow loss in the blade tip and hub ; the feasibility and high efficiency of this procedure has been verified by the tests of the prototype fan ; a new computer - aided 3d blading is used to optimize the blade ; numerical inverse checking is adopted to enhance accuracy in designing and cut down the period of the designing and production. this design system can make the optimized blade with " forward inclination ", " inclining sweep ", " bending sweep ", to minimize the various secondary flow losses, to expand the steady working range of the fan, and to suppress the aerodynamic noise source

    本文通過對一種新型高性能礦用局部通風機設計、製造及試驗全過程綜述,展現了新先進設計體系在民用通風機上成功運用,其研製特是: ( 1 )在葉片氣動設計中為了葉根及葉尖區二次流損失,採用可控渦扭向規律設計,樣機實測高性能驗證了這種方法可行性和高效性; ( 2 )在設計方法中採用較精確數值反驗算,獲取最優設計方案,大大提高設計準確性和成功率,並縮短了設計試制周期; ( 3 )在設計過程中發展了計算機輔助三維葉片造型新方法,可以根據設計需要簡便快捷地對葉片進行「前」 、 「掠」或「彎掠」造型,這些造型對減小各種二次流損失、擴大穩定工況范圍和控制葉輪機氣動噪聲源起到了非常好作用。
  4. Abstract : a new aerodynamic design system developed by authors for draft fan with enhanced efficiency, suppressed noise, enlarged flux and high load. the new design system features : a twist regulation for vortex control is employed in designing to lessen the secondary flow loss in the blade tip and hub ; the feasibility and high efficiency of this procedure has been verified by the tests of the prototype fan ; a new computer - aided 3d blading is used to optimize the blade ; numerical inverse checking is adopted to enhance accuracy in designing and cut down the period of the designing and production. this design system can make the optimized blade with " forward inclination ", " inclining sweep ", " bending sweep ", to minimize the various secondary flow losses, to expand the steady working range of the fan, and to suppress the aerodynamic noise source

    文摘:本文通過對一種新型高性能礦用局部通風機設計、製造及試驗全過程綜述,展現了新先進設計體系在民用通風機上成功運用,其研製特是: ( 1 )在葉片氣動設計中為了葉根及葉尖區二次流損失,採用可控渦扭向規律設計,樣機實測高性能驗證了這種方法可行性和高效性; ( 2 )在設計方法中採用較精確數值反驗算,獲取最優設計方案,大大提高設計準確性和成功率,並縮短了設計試制周期; ( 3 )在設計過程中發展了計算機輔助三維葉片造型新方法,可以根據設計需要簡便快捷地對葉片進行「前」 、 「掠」或「彎掠」造型,這些造型對減小各種二次流損失、擴大穩定工況范圍和控制葉輪機氣動噪聲源起到了非常好作用。
  5. Improvement of barrier protection performance was analyzed from views of material, structure and type, installation of concrete barrier. it was presented to increase the protection capacity of the barrier through material improvement so as to decrease rigidity of the barrier. the effect that the height of the point of intersection between the up and below inclined plane may have on car overturn after impact

    從混凝土護欄材料、結構形式、施工方法等方面進行了護欄防護性改進分析,提出通過改進材料來提高護欄防護性,護欄剛度,討論了護欄截面上、下斜面交叉高度對車輛碰撞后翻可能性影響。
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