作者: Eugene S Love
DOI:
关键词: Simple (abstract algebra) 、 Shock wave 、 Range (statistics) 、 Hypersonic flow 、 Structural engineering 、 Aerodynamics 、 Computational fluid dynamics 、 Mechanics 、 Choked flow 、 Mach number 、 Engineering
摘要: A reexamination has been made of the use simple concepts for predicting shape and location detached shock waves. The results show that modifications existing methods can yield good predictions many nose shapes a wide range Mach numbers.