Direct Numerical Simulations of Transonic Flow Around an Airfoil at Moderate Reynolds Numbers
Direct Numerical Simulations of Transonic Flow Around an Airfoil at Moderate Reynolds Numbers
复制标题
DOI:
10.2514/1.j057335
复制
发表时间:
2019-01
期刊:
影响因子:
2.5
通讯作者:
M. Zauner;N. Tullio;N. Sandham
中科院分区:
文献类型:
--
作者:
M. Zauner;N. Tullio;N. Sandham
To reduce friction and wave drag on the wings of more-efficient next-generation aircraft, it is important to understand laminar–turbulent boundary-layer transition and shock-wave interactions. In t...