光学精密工程2026，Vol.34Issue(1)：98-111,14.DOI:10.37188/OPE.20263401.0098
涵道式飞行汽车螺旋桨的气动特性与涵道外形设计
Aerodynamic characteristics and ducted shape design of ducted flying car propeller
摘要
Abstract
To design a ducted propeller that satisfies the requirement for high thrust efficiency during hover in a ducted flying car,a dedicated design methodology is proposed.Blade geometry is developed using blade element momentum theory in conjunction with ducted propeller vortex theory,and the resulting de-signs are refined through CFD-based corrections to meet target performance.Under hover conditions,the aerodynamic performance of the ducted propeller is evaluated and compared with that of an isolated propel-ler.The results indicate that,due to suppression of blade-tip vortices and the additional lift generated by the duct,total thrust is increased by 11.1%while power consumption is reduced by 10.5%relative to the isolated propeller.To further enhance hover performance,an innovative variable-duct propeller configura-tion is proposed,in which the flare expansion angle is dynamically adjusted to maximize inlet airflow dur-ing hover,yielding a 15.53%increase in total thrust.The study validates a high-accuracy design frame-work that integrates blade element momentum theory with CFD correction,providing theoretical and tech-nical support for efficient aerodynamic design of propulsion systems for flying vehicles.关键词
飞行汽车/涵道螺旋桨/叶素动量理论/数值仿真/气动特性/可变涵道设计Key words
flying car/ducted propeller/blade element momentum theory/numerical simulation/aero-dynamic characteristic/variable duct design分类
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张增奎,李京阳,印明威,郝文乾,谢佳苗,王哲,高舒煜..涵道式飞行汽车螺旋桨的气动特性与涵道外形设计[J].光学精密工程,2026,34(1):98-111,14.基金项目
国家自然科学基金资助项目(No.11602123) （No.11602123）
内蒙古自治区杰出青年培育基金资助项目(No.2019JQ002) （No.2019JQ002）
