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experimental research on aero-propulsion coupling characteristics of a distributed electric propulsion aircraft

Chinese Journal of Aeronautics 2023年第2期36卷 201-212页

作者： Xingyu ZHANG Wei ZHANG Weilin LI Xiaobin ZHANG Tao LEI School of Aeronautics Northwestern Polytechnical UniversityXi'an 710072China Key Laboratory of Aircraft Electric Propulsion Technology Ministry of Industry and Information TechnologyXi'an 710072China School of Automation Northwestern Polytechnical UniversityXi'an 710072China

Distributed Electric Propulsion(DEP)aircraft use multiple electric motors to drive the propulsors,which gives potential benefits to aerodynamic-propulsion interaction.To investigate and quantify the aerodynamic-propulsion interaction effect of the wing section,we built a DEP demonstrator with 24"high-lift"Electric Ducted Fans(EDFs)distributed along the wing’s trailing edge.This paper explores and compares the aero-propulsion coupling characteristics under various upstream speed,throttle,and EDF mounting surface deflection angles using a series of wind tunnel tests.We compare various lift-augmentation power conditions to the clean configuration without propulsion unit under the experiment condition of 15-25 m/s freestream flow and angles of attack from-4°to 16°.The comparison of computational results to the experimental results verifies the effectiveness of the computational fluid dynamic analysis method and the modeling method for the DEP configuration.The results show that the EDFs can produce significant lift increment and drag reduction simultaneously,which is accordant with the potential benefit of Boundary Layer Ingestion(BLI)at low airspeed.

关键词： Aero-propulsion coupling Boundary layer ingestion Distributed electric propulsion Short Take-Off and Landing(STOL) wind-tunnel experiment

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Influence of wind Deviation Angle on n-Hexane Evaporation Loss of Internal Floating-Roof Tanks

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China Petroleum Processing & Petrochemical Technology 2020年第2期22卷 46-55页

作者： Huang Weiqiu Xu Manlin Li Fei Ji Hong Fang Jie Jiangsu Key Laboratory of Oil&Gas Storage and Transportation Technology Changzhou UniversityChangzhou 213164

With the increasing attention to environmental protection,it is still necessary to strictly control the oil evaporation loss from the IFRT(internal floating-roof tank)to the atmosphere.Upon using n-hexane as a representative of light oil,the effects of the WDAs(wind deviation angles)on airflow distribution,the wind speed,the n-hexane vapor concentration,and the evaporation loss rate in the IFRT were investigated,and the mass transfer of the vapor-air was analyzed.The results are shown as follows:when the WDA is 0°,the vapor concentration in the gas space above the floating deck is the lowest;when the WDA is 22.5°,the oil evaporation loss rate is the largest;when the WDA is 45°,the vapor concentration is the highest,but the evaporation loss rate is the smallest.It is recommended to arrange the vent to the wind direction with an angle of 45°to reduce the evaporation loss and protect the atmospheric environment.

关键词： wind deviation angle n-hexane evaporation loss internal floating-roof tank numerical simulation wind-tunnel experiment

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