outlet section 中文意思是什麼
outlet section
解釋
出流斷面-
In low mass flux and high outlet quality conditions, experiments have been performed using vertical heated tube, cooled by water, to determine chf value for a uniformly heated section
針對低流量高含汽量工況，本論文試驗在長度為2 . 1m ，管徑為0 . 014m的均勻受熱圓管中得到93組chf數據。 -
There are several important issues to that attention should be paid in the design of test bed, such as the measurement of the temperature difference between the inlet and outlet of test section and the temperature of cooling water in the inlet and outlet of condensing tubes, filled volume of the steam boiler and its level control, the determination of the natural acting head of high temperature tank and design of the cooling water flow of measuring tank
試驗臺由高溫工質自然循環子系統、冷卻水機械循環子系統和計算機監測控制子系統構成，試驗段進出口溫差及冷凝管進出口溫度的測試、蒸汽鍋爐充注量及液位控制、高溫水箱自然作用水頭的設計、冷卻水流量計量水箱的設計等是試驗臺設計中值得重視的問題。 -
Works fechnique the power is strong, produce the equipment excellent, the examination way assort, and the main product adopt the oil ( air ) mouth of well the apparatus, artesian well the fube concourse, and all pass the section of national authority direct to inspect qualified, the business enterprise passed the iso9001 the attestation of international mass system, and carry through whole management process, and guarantee out the plant product 100 % of proplar and national and each and big oil - field of superior quality, producl, and outlet kazakhstan, egypt iso - nation
工廠技術力量雄厚、生產設備精良、檢測手段齊全，主產品採油氣井口裝置、鉆井管匯，均通過國家權威監督部門檢驗合格，企業通過了iso9001國際質量體系認證，並貫徹整個管理過程，保證出廠產品100 %的優質，產品暢銷全國各大油田，並出口哈薩克斯坦、埃及等國家。 -
The effect of secondary fuel nozzle location, the mass flow rate of secondary fuel and outlet area of ejectorjet were studied. the main results are : the geometry structure of ejectorjet can be compatible with other rbcc operation modes by secondary combustion organization ; the distribution of secondary fuel on ejectorjet cross section is significant for secondary combustion stability. spi combustion organization method is promising
實驗研究了二次燃料噴注位置、二次燃料噴注量、后體出口面積對引射火箭性能的影響，得到的結論為：通過燃燒組織，引射火箭模態可以和其他工作模態（亞燃超燃）共用燃燒室而不需做大的幾何變化；二次燃料在引射火箭通道截面上的分佈對于引射火箭的穩定工作有重要意義。
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