Research on the Servo Loading Systems of High Aspect Ratio Wing Test

It occurs that the loading point changes with the test piece in the aircraft structure test. In particularly, the large deformation of the wing will cause the issue that loading point is not perpendicular with the plan of the wing. A kind of servo loading systems is applied in composite material win...

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Bibliographic Details
Main Authors: Li Xiaohuan, Zhang Lei
Format: Article
Language:zho
Published: Editorial Department of Advances in Aeronautical Science and Engineering 2019-04-01
Series:Hangkong gongcheng jinzhan
Subjects:
Online Access:http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2018051?st=article_issue