Research on aerodynamic applied technique

2012-01-13 | admin

◆  Flow control and application

◆  Water / gas interface research and application

◆  Research on supersonic combusion mechanism

◆  Research on supersonic engine technique

Research on Supersonic Flow Mechanism

Interference on Control Rudder by Jet Flow            Separate Shockwave Weaken by Porous Wall

Three-dimensional Hypersonic Shockwave Structure on Vapor Screen