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转子翼驱动功率与升/阻力特性研究

梁利华 姜寅令 史洪宇 李剑峰

哈尔滨工程大学学报2023,Vol.55Issue(10):1705-1711,7.
哈尔滨工程大学学报2023,Vol.55Issue(10):1705-1711,7.DOI:10.11990/jheu.202110002

转子翼驱动功率与升/阻力特性研究

Driving power and lift/drag characteristics of rotor swings

梁利华 1姜寅令 2史洪宇 1李剑峰1

作者信息

  • 1. 哈尔滨工程大学 智能科学与工程学院,黑龙江 哈尔滨 150001
  • 2. 哈尔滨工程大学 智能科学与工程学院,黑龙江 哈尔滨 150001||东北石油大学 电气信息工程学院,黑龙江 大庆 163318
  • 折叠

摘要

Abstract

This paper proposed a method for calculating the drive power of a servo system based on the dynamic fluid torque and average angular velocity on the rotor wing to investigate the driving power of the new Magnus rotor-type anti-rolling device(rotor wing).First,we conducted three-dimensional transient simulations on a rotor swing using the soft ANSYS-Fluent,obtaining the hydrodynamic characteristics during the rolling period.Then,according to the dynamic fluid force and the angular velocity of the rotor,we obtained the total torque on the rotor wing,including inertial torque,friction torque,and viscous resistance torque.The results showed that the average lift-to-drag ratio was greater than 4 at a sailing speed of 7 knots for a rotor wing with a length of 3 m and a diameter of 0.4 m.The rotor wing can also generate sufficient lift at low speeds.Furthermore,the lift per unit projected area of the rotor wing was greater than traditional fins,whereas the opposite result was obtained for drag.Finally,the driving power of a rotor wing is less than that of a traditional stabilizing fin.

关键词

转子翼/Magnus效应/船舶减摇/升/阻力特性/驱动功率/CFD仿真/减摇鳍/ANSYS软件

Key words

rotor wing/Magnus effect/roll stabilization/lift/drag characteristics/driving power/computational fluid dynamics simulation/fin stabilizer/ANSYS software

分类

信息技术与安全科学

引用本文复制引用

梁利华,姜寅令,史洪宇,李剑峰..转子翼驱动功率与升/阻力特性研究[J].哈尔滨工程大学学报,2023,55(10):1705-1711,7.

基金项目

国家自然科学基金(U20A20187) (U20A20187)

"兴辽英才计划"项目(XLYC2007087) (XLYC2007087)

哈尔滨工程大学学报

OA北大核心CSCDCSTPCD

1006-7043

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