机身
变形(气象学)
飞行试验
工程类
结构工程
流离失所(心理学)
组分(热力学)
飞行操纵面
汽车工程
海洋工程
航空航天工程
计算机科学
空气动力学
地质学
物理
海洋学
热力学
心理治疗师
心理学
作者
Zbigniew Czyż,Patryk Jakubczak,Piotr Podolak,Krzysztof Skiba,Paweł Karpiński,Magda Droździel-Jurkiewicz,M. Wendeker
摘要
The paper presents the authors’ method and test rig for performing the deformation analysis of unmanned aircraft fuselages. To conduct the analysis, the DIC system was used, as well as a test rig designed and constructed by the authors, equipped with a dedicated control and load control system. The article presents a description of the research capabilities of the test rig developed for testing the deformation of unmanned aircraft fuselages. Due to the specific operating conditions of the designed fuselage, the test rig developed allows the simulation of loads corresponding to different flight conditions. In addition, it is possible to change the forces acting on the fuselage simultaneously for all servos or each of them separately. Finally, results showing the displacement of component control points for the considered fuselage versions are presented. The tests carried out using the developed test rig allowed the verification of the maximum deformations.
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