首页>
外国专利>
Method of and apparatus for preventing leading edge shocks and shock- related noise in transonic and supersonic rotor blades and the like
Method of and apparatus for preventing leading edge shocks and shock- related noise in transonic and supersonic rotor blades and the like
展开▼
机译:防止跨音速和超音速转子叶片等中前缘冲击和与冲击相关的噪声的方法和装置
展开▼
页面导航
摘要
著录项
相似文献
摘要
This disclosure is concerned with novel rotor blade and similar foil designs that, by critical skewing of intermediate blade regions where the airflow is supersonic, prevents leading edge shocks and shock-related noise.
展开▼