首页> 外文期刊>Journal of Mechanical Science and Technology >Performance improvement of weis-fogh type ship’s propulsion mechanism using rubber type elastic wing
【24h】

Performance improvement of weis-fogh type ship’s propulsion mechanism using rubber type elastic wing

机译:橡胶型弹性机翼改善魏斯福型舰船的推进性能

获取原文
获取原文并翻译 | 示例
           

摘要

The performance improvement for a propulsion mechanism of Weis-Fogh type was attempted by using an elastic rubber wing. The elastic wings were made of rubber and wood with the rubber rate of 0%, 25%, and 50% in the wing area. The thrust and drag on the wing were measured for various velocity ratio V/U, opening angles of α=15° and α=30°. The average thrust coefficient and average thrust efficiency of the elastic wing were increased compared to those of the rigid wing, and the average drag coefficient was decreased; overall, by using elastic wing, the thrust, drag, and efficiency characteristics were improved. For an elastic wing with opening angle α=15° and rubber rate Rs=50% which relatively had the greatest performance improvement, thrust coefficient was increased by 30%, drag coefficient was decreased by 21%, and propulsive efficiency was increased by 17% in average compared to the rigid wing with Rs=0%.
机译:试图通过使用弹性橡胶翼来改善Weis-Fogh型推进机构的性能。弹性机翼由橡胶和木材制成,机翼区域的橡胶率为0%,25%和50%。测量了各种速度比V / U,α= 15°和α= 30°的开度时机翼上的推力和阻力。与刚性翼相比,弹性翼的平均推力系数和平均推力效率增加,而平均阻力系数减小;总体而言,通过使用弹性机翼,推力,阻力和效率特性得到了改善。对于相对具有最大性能改进的张开角α= 15°和橡胶比率Rs = 50%的弹性机翼,推力系数增加30%,阻力系数减少21%,推进效率增加17%平均而言,与Rs = 0%的刚性机翼相比。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号