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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