国家数值风洞(NNW)工程在高超声速中的应用研究进展

doi:10.7527/S1000-6893.2021.25746

Abstract

Abstract: With the fast development of CFD techniques in recent years, CFD numerical simulation software has been widely used in the development of aircrafts, and plays an increasingly important role in most stages of aerospace and other fields. The National Numerical Windtunnel (NNW) Project adheres to the principle of "using while building". By integrating the software of structural mechanics, flight mechanics, engineering thermodynamics, acoustics, optics, electromagnetics, multiphase fluid mechanics and other disciplines, the project is playing an active role in aerospace, transportation, energy and power, environmental protection and disaster mitigation, and other disciplines. This paper summarizes the achievements of using the NNW software for hypersonic boundary layer transition, turbulence and high-order schemes. Development of applicaion of the NNW software for the problems of complex flow interaction, dynamic stability and multidisciplinary coupling simulation is also discussed. Cases are displayed to demonstrate the functions and characteristics of NNW software, so as to boost the spread and application of the software nationwide.

Key words: National Numerical Windtunnel (NNW) Project, transition, turbulent flow, hypersonic, dynamic stablity, aeroservo elasticity

CLC Number:

V211.3

CHEN Qi, CHEN Jianqiang, YUAN Xianxu, GUO Qilong, WAN Zhao, QIU Bo, LI Chen, ZHANG Yifeng. Progress on application of National Numerical Windtunnel Project for hypersonic[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(9): 625746-625746.

References

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Progress on application of National Numerical Windtunnel Project for hypersonic

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