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多层合采油藏油水井产量劈分原理及应用 被引量:12
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作者 李成勇 柳金城 +2 位作者 李晓茹 叶慧平 丁晓军 《大庆石油地质与开发》 CAS CSCD 北大核心 2010年第1期55-59,共5页
注水开发油田进入高含水期后,开发矛盾日益突出,稳产的形势较严峻,剩余油在空间上分布十分复杂,挖潜难度越来越大,油田必须要走精细开发的路子,而油水井产量劈分是多层油藏精细开发的基础。从渗流力学基本理论出发,建立多层合采... 注水开发油田进入高含水期后,开发矛盾日益突出,稳产的形势较严峻,剩余油在空间上分布十分复杂,挖潜难度越来越大,油田必须要走精细开发的路子,而油水井产量劈分是多层油藏精细开发的基础。从渗流力学基本理论出发,建立多层合采井分层流量计算理论模型,分析各因素对分层流量变化规律的影响;并在理论研究基础上,结合油田开发的实际情况,提出了油水井产量劈分的具体指导原则,对现场多层合采油井产量进行了劈分工作。对于油田精细开发具有一定的指导意义。 展开更多
关键词 渗流 产量劈分 多层合采 层面流量
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Study on the distribution of strata rock temperature around a driving head with auxiliary ventilation
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作者 高建良 《Journal of Coal Science & Engineering(China)》 2004年第2期50-54,共5页
The distributions of strata rock temperature around a driving head with auxil- iary ventilation were analyzed theoretically based on a program which was developed by the authors to predict the thermal environmental co... The distributions of strata rock temperature around a driving head with auxil- iary ventilation were analyzed theoretically based on a program which was developed by the authors to predict the thermal environmental conditions in a development heading with forcing auxiliary ventilation. The influences of wetness of the airway surface were dis- cussed on the cooled zone of the strata rock and on the temperature distribution in the surrounding rock. It is shown that the advancing speed and driving time have little influ- ence on the temperature profile in front of the working face of a driving airway, and the rock temperature 1.5 m ahead of the working face can be taken as the virgin rock tem- perature. 展开更多
关键词 auxiliary ventilation working face strata rock temperature heat flux
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Boundary Layer Development on a Concave Surface: Flow Visualization and Hot Wire Velocity Measurements
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作者 Farouk Hachem Mahmoud Khaled Mohamad Ramadan Charbel Habchi 《Journal of Energy and Power Engineering》 2014年第7期1177-1182,共6页
Gortler vortices are key issues in the design of gas turbine blades. The present study deals with flow visualization over concave surface for gas turbine applications. The aim is to comprehend qualitatively the flow t... Gortler vortices are key issues in the design of gas turbine blades. The present study deals with flow visualization over concave surface for gas turbine applications. The aim is to comprehend qualitatively the flow trends, particularly the Gortler vortices formation and development. Gortler vortices have the shape of mushroom-like vortices regularly spaced at 25 mm. These vortices grow and increase in strength more rapidly along the surface in the case of the same grid of turbulence applied to the measuring section. The curvature radius of the studied blade is 0.5 m and the stream turbulence intensity level is 2.6%. The velocity field is measured by hot wire anemometer in the streamwise direction. The velocity profile is found to be highly distorted by the momentum transfer associated with Gortler vortices. The results are compared to Blasius flow and to literature data for a blade with curvature radius equal to 2 m. 展开更多
关键词 Gortler vortices concave surface flow visualization velocity profile gas turbine.
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Skin Friction Gage for Measurements in Hypersonic Flow
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作者 Francois Falempin Marat Goldfeld Roman Nestoulia 《Journal of Thermal Science》 SCIE EI CAS CSCD 2003年第1期44-50,共7页
A description and results of tests of a new small-scale gage for direct measurement of skin friction force are presented in the paper.The gage design provides separated measurement of longitudinal and transversal comp... A description and results of tests of a new small-scale gage for direct measurement of skin friction force are presented in the paper.The gage design provides separated measurement of longitudinal and transversal component of friction force.Application of this scheme provides high sensitivity and necessary high-frequency response of the gage.The tests of the gage were carried out in a blow down wind tunnel at Mach numbers of 2 and 4 within the range of Reynolds numbers Rex from 0.8 to 5 million and in the hot-shot wind tunnel at Mach number 6 and Reynolds numbers Rex=2.5-10 million.The measurements of skin friction were carried out on a flat plate and on a ramp beyond the shock wave.Simultaneously with the direct measurement of friction in the blow down wind tunnel,the measurements of profiles of average velocities and mass flow rate pulsations were realised.Analysis of measurement errors has shown that the friction gage permits to measure skin friction coefficient on a flat plate with mistake not more than 10%. 展开更多
关键词 skin friction gage hypersonic flow scramjet.
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