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Study on Flight Load Modeling Method for Complex Structure Aircraft

The traditional flight load modeling method of complex structure aircraft has the problems of large error and low efficiency. A flight load improved modeling method is proposed,which is comprehensively considering the influence of the bridge index and load equation index on the load model. Taking th...

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Збережено в:
Бібліографічні деталі
Автори: CHEN Zhiming, TANG Ning, FAN Huafei
Формат: Artigo
Мова:Chinês
Опубліковано: Editorial Department of Advances in Aeronautical Science and Engineering 2022-04-01
Серія:Hangkong gongcheng jinzhan
Предмети:
Онлайн доступ:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2021139?st=article_issue
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