首页> 美国政府科技报告 >Effect of a Rotating Propeller on the Separation Angle of Attack and Distortionin Ducted Propeller Inlets
【24h】

Effect of a Rotating Propeller on the Separation Angle of Attack and Distortionin Ducted Propeller Inlets

机译:旋转螺旋桨对导管螺旋桨进气道分离角和畸变的影响

获取原文

摘要

The present study represents an extension of an earlier wind tunnel experimentperformed with the P&W 17-in. Advanced Ducted Propeller (ADP) Simulator operating at Mach 0.2. In order to study the effects of a rotating propeller on the inlet

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