翼部層 的英文怎麼說
中文拼音 [yìbùcéng]
翼部層
英文
flank bed-
In qiaokou area, deep parts of well qiaol4, 20, 23, 25, 60 are related to source rock in gegangji sag, while crude oil in well qiao38 is related to source rock in qianliyuan sag ; in baimiao structure, crude oil in well bail2 is related to source rock of es33 - es34 in qianliyuan sag, while condensate in well bai54, 17, 9 is related to source rock of es32 in qianliyuan sag and crude oil in well bai6 is from oil kitchen gegangji. the study on illite age testing, inclusion enclave temperature testing and saturation pressure testing has been used to know the time of the deeply buried gas net pay formed. the time of the deeply buried gas net pay formed can be divided into two stages
油源對比結果表明杜寨地區濮深15井的凝析油來源於本區es _ 3 ~ 3 es _ 3 ~ 4地層，前8井es _ 3 ~ 2原油來源es _ 3 ~ 2地層；橋口地區東翼葛崗集窪陷一側的橋14 、 20 、 23 、 25 、 60井深層油氣與葛崗集窪陷烴源巖有關，橋口壘塊橋38井原油與前梨園窪陷烴源巖有關；白廟構造翼部白12井原油主要與前梨園窪陷es _ 3 ~ 3 es _ 3 ~ 4段烴源巖有關，構造腰部白54 、 17 、 9等井的凝析油與前梨園窪陷es _ 3 ~ 2段烴源巖有關，白16井原油來源於葛崗集生油窪陷。The tectonic style inside the basin is characterized by occurrence of anticlines from the margins to center of the basin, with two limbs mostly starting from reverse faults, developing a tectonic pattern of two faults sandwiching an uplift
盆地內部的構造樣式以自盆地邊緣至中心以此形成背斜構造為顯著特徵，背斜兩翼多發育逆斷層，構成「兩斷夾一隆」的構造格局。In order to predict hydrodynamic characteristics a computational system is developed including determination of the pressure distribution on a wing section by use of the conformal mapping method and panel method respectively and of the flow in boundary layer according to the thin shear layer approximation ( tsl ) for navier - stokes equation approach. the wing sections of naca4412 and naca0012 are applied to test the computational system. the numerical inspection shows that the panel method with better precision and the momentum and the displacement thickness of boundary layer can be used to complete this calculation
本文分別用守屋的保角變換法和基於源匯渦分佈的面元法，建立了計算槳葉表面壓力分佈的數學模型；應用納維-斯托克方程的薄層近似理論模式和有限差分數值方法，建立了計算機翼表面邊界層內部流動的數學模型；應用槳葉表面邊界層內部粘性流動和外部勢流流動在邊界上的匹配演算法，建立了槳葉表面二相流流動的計算方法和相應的計算機程序。The space shutter colombia just centigrated re - entry upon ( columbia disintegrated upon re - entry into ) earth ' s atmosphere on february 2003, after degrade puncture indolesia ( debris punctured the orbiter ' s insulation ) allow superheating gases penetrated its wing, the disaster shuttle killed 7 astronaunt
2003年2月哥倫比亞號航天飛機進入大氣層以後就解體了，有碎片刺穿了航天飛機的絕緣層，使過熱氣體進入了機翼，這場災難使航天飛機中的7名宇航員全部遇難。Through reservoir prediction, it indicated that the reservoir in mainan structure and mopan - laowan buried structure which located in short limb and bottom wall were finely developed, this two areas were the primary area for the further exploration and drill site design in dachiganjing structural belt
通過儲層橫向預測，發現麥南構造和陡翼斷層下盤的磨盤老灣潛伏構造儲層較發育，是大池乾井構造帶下一步勘探及井位部署的重點區域。On the background of aeronautics and astronautics requirement, along with the line of modularization of fiber optic smart structure, aimed at the safety matter of aerofoil pivotal parts, build optic fiber smart layer self - diagnosing system
以航空航天需求為背景，以光纖智能結構的集成為主線，針對飛機機翼關鍵部件安全性問題，建立了基於光纖智能夾層的自診斷系統。3. the characteristics of boundary layer ' s transition, shape and separation are researched. the details as follows : ( l ) airfoil surface is turbulent boundary layer flows ; ( 2 ) velocity figure changed unsteady near the point of boundary layer separation due to randomicity of turbulent flow ; ( 3 ) the airfoil have better state of boundary layer separation and poor stall characteristics because of the upper surface of airfoil is flat
給出了該翼型的附面層特性：翼型表面基本為湍流附面層；在靠近附面層分離位置處，速度型形狀、特別是靠近翼型表面的底部速度型形狀變化不定，是湍流流動的隨機性所致；該翼型具有較好的附面層分離形態，但在失速迎角附近，附面層分離形態變化劇烈、失速特性差，是翼型上翼面形狀較為平坦所致。分享友人