Near space hypersonic vehicle has the advantages of fast speed, moderate height, fast military response and strong penetration resistance. It has attracted the attention of major powers in the world, and become the research frontier in aerospace field. The research team of SAA of ZJU has participated in multiple national major projects in recent years, systematically established the hypersonic thermochemical nonequilibrium flow moment theory and the related calculation method, formed the hypersonic aerodynamic characteristics calculation, aerodynamic design and optimization, the hybrid network unsteady aerodynamic calculation and other software systems with independent intellectual property rights.They are widely applied to aerodynamic characteristics analysis, aerodynamic layout design and optimization, hypersonic plasma flow modeling and analysis, pneumatic optical effect and physical, and other researches.
