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Numerical and Experimental Analysis of A Ducted Propeller Designed by A Fully Automated Optimization Process Under Open Water Condition 被引量:1
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作者 余龙 Markus DRUCKENBROD +2 位作者 Martin GREVE 王珂琦 Moustafa ABDEL-MAKSOUD 《China Ocean Engineering》 SCIE EI CSCD 2015年第5期733-744,共12页
A fully automated optimization process is provided for the design of ducted propellers under open water conditions, including 3D geometry modeling, meshing, optimization algorithm and CFD analysis techniques. The deve... A fully automated optimization process is provided for the design of ducted propellers under open water conditions, including 3D geometry modeling, meshing, optimization algorithm and CFD analysis techniques. The developed process allows the direct integration of a RANSE solver in the design stage. A practical ducted propeller design case study is carried out for validation. Numerical simulations and open water tests are fulfilled and proved that the optimum ducted propeller improves hydrodynamic performance as predicted. 展开更多
关键词 ducted propeller optimum design RANSE solver automatic optimization method
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Aerodynamic design of tractor propeller for high-performance distributed electric propulsion aircraft 被引量:5
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作者 Kelei WANG Zhou ZHOU +1 位作者 Zhongyun FAN Jiahao GUO 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2021年第10期20-35,共16页
Aiming to maximize the aerodynamic performance of the Distributed Electric Propulsion(DEP)aircraft,a hybrid design framework which focuses on the aerodynamic performance of the propeller/wing integration has been deve... Aiming to maximize the aerodynamic performance of the Distributed Electric Propulsion(DEP)aircraft,a hybrid design framework which focuses on the aerodynamic performance of the propeller/wing integration has been developed and validated numerically.Variable-fidelity modelling for propeller aerodynamics has been used to achieve computational efficiency with reasonable accuracy.By optimizing the aerodynamic loading distributions on the tractor propeller disk,the induced slipstream is redistributed into a form that is beneficial for the wing downstream,based on which the propeller blade geometry is generated through a rapid inversed design procedure.As compared with the Minimum Induced Loss(MIL)propeller at a specified thrust level,significant improvements of both the lift-to-drag ratio of the wing and the propeller/wing integrated aerodynamic efficiency is achieved,which shows great promise to deliver aerodynamic benefits for the wing within the propeller slipstream without any additional devices. 展开更多
关键词 Aerodynamic loading distributions Aerodynamic performance Distributed electric propulsion Hybrid design framework Propeller/wing integration Variable-fidelity propeller modelling and aerodynamic analyses methods
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