当前位置: X-MOL 学术J. Aerosp. Eng. › 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.)
Aeroelastic Damping Estimation for a Flexible High-Aspect-Ratio Wing
Journal of Aerospace Engineering ( IF 2.4 ) Pub Date : 2021-12-21 , DOI: 10.1061/(asce)as.1943-5525.0001390
Ilias Tsatsas 1 , Alessandro Pontillo 2 , Mudassir Lone 3
Affiliation  

Estimation of aeroelastic damping for a very flexible high-aspect-ratio wing using wind-tunnel test data is presented in this work through the comparison of four different methods: half-power, half-quadratic gain, an adapted version of random ...

中文翻译:

柔性大展弦比机翼的气动弹性阻尼估计

在这项工作中,通过对四种不同方法的比较,介绍了使用风洞测试数据估算非常灵活的高展弦比机翼的气动弹性阻尼:半功率、半二次增益、随机...
更新日期:2021-12-22
down
wechat
bug