Research status of electron beam plasma for aerodynamic applications in China

摘要

Recently, many aerodynamic problems are arising under the quickly developments of supersonic and hypersonic flight ve hides, such as boundary layer separation, flight drag force in creasing, etc. Differencing with the passive flow control methods, the active method attracts more and more attention and becomes one of the most booming realms of aerodynamics. Among kinds of methods, the approach of non-equilibrium plasma is the most prospective one due to its fast reaction time, lo w device weight and size.