Theoretical Prediction of Roll Moment Due to Sideslip for Thin Low-Aspect-Ratio Wings

Theoretical Prediction of Roll Moment Due to Sideslip for Thin Low-Aspect-Ratio Wings
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DOI:
10.2514/1.j057160
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发表时间:
2019-03
期刊:
影响因子:
2.5
通讯作者:
Thomas Linehan;K. Mohseni
Thomas Linehan;K. Mohseni
中科院分区:
工程技术3区
文献类型:
--
作者:
Thomas Linehan;K. Mohseni

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