当前位置: X-MOL 学术AIAA J. › 论文详情
Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)
Wall Pressure Fluctuations Beneath Hypersonic Boundary Layer over Plate
AIAA Journal ( IF 2.5 ) Pub Date : 2020-11-24 , DOI: 10.2514/1.j059882
XiaoJian Zhao 1 , Lei Zhao 2
Affiliation  

Wall pressure fluctuations beneath a boundary layer are the main cause of structural vibration for hypersonic aircraft. To accurately predict the load environment of pressure fluctuations, a measur...

中文翻译:

板上方高超声速边界层下方的壁面压力波动

边界层下方的壁面压力波动是高超音速飞机结构振动的主要原因。为了准确预测压力波动的负载环境,一种测量...
更新日期:2020-11-24
down
wechat
bug