靜壓損失 的英文怎麼說

中文拼音 [jìngsǔnshī]
靜壓損失 英文
static pressure loss
  • : 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
  • : 壓構詞成分。
  • : Ⅰ動詞1 (減少) decrease; lose 2 (損害) harm; damage 3 [方言] (用尖刻的話挖苦人) speak sarcas...
  • 損失 : 1. (失去) lose 2. (失去的東西) loss; wastage
  1. Information technology - lossless and near - lossless compression of continuous - tone still images : baseline

    信息技術.連續音調止圖像的無和接近無縮.基線
  2. Information technology - lossless and near - lossless compression of continuous - tone still images - part 2 : extensions

    信息技術.連續影調止圖像的無和接近無縮.第2部分:擴充部分
  3. Abstract : optimum distances between primary nozzle exit and mixing tube inlet, static pressure recovery of the mixing flow in mixing tube 、 total pressure distributions at the exit of mixing tube 、 pumping coefficients and total pressure losses of the exhaust ejector systems with four different types of primary nozzles have been measured in the experiments

    文摘:對4種主噴管組成的排氣引射系統的引射系數和總、各主噴管出口與混合管進口之間的最佳間距、混合氣流在混合管內的恢復及混合氣流在混合管出口處的總分佈等進行了測量和對比。
  4. At quiescent conditions, the power supply voltage appears on the plate ( minus a little loss due to the ir loss in the transformer

    態條件下,高直接加載在屏級上(減去一點在變器初級的直流電阻上的) 。
  5. Measured hole mass flows and a constant static pressure mixing analysis, together with the measured losses, allowed the decomposition of the losses into three distinct entropy generation mechanisms : loss generation within the hole, loss generation due to the mixing of the coolant with the mainstream, and change in secondary loss generation in the " blade passage

    論文還進行了葉片冷卻孔質量流的測量與常氣流混合分析,結合前述氣動力和冷卻空氣耗的測量結果表明,端壁氣膜冷卻的綜合明顯地由三個部分組成:葉片冷卻孔內產生的;由於冷卻空氣與主流熱空氣的混合產生的;二次流的變化產生的
  6. 6 fume hood shall be designed to minimize static pressure loss. bell shaped exhaust collar configuration shall be provided

    通風櫃的設計要減少靜壓損失。因此一般在排氣口附件採用鐘型設計。
  7. Results from this investigation show that the loss generation within the coolant holes is substantial and that ejection into regions of low static pressure increases the loss per unit coolant mass flow. the results also reveal strong interactions between endwall coolant ejection and secondary flow in the blade passage. the secondary flow has a strong influence on coolant trajectories and coolant ejection delays the three - dimensional separation of the inlet boundary layer on the endwall, chang the secondary flow and reduces its associated losses

    本文的研究成果顯示,冷卻孔內產生的是主要的,並且低區域的冷空氣噴射會增加單位冷空氣質量流的消耗;噴射的冷空氣與葉柵端壁流場之間有強烈的相互作用;二次流對冷卻空氣的流動軌跡有較強的影響;冷空氣噴射能延緩端壁入口邊界層的三維分離、改變二次流從而減少其相關耗。
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