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Discussion of Speeding Up Fatigue Test of Full-Scale Aircraft
Engineering ProceedingsThe full-scale aircraft fatigue test is a critical assessment and validation of the fatigue and damage tolerance design of new aircraft models, and it is also a prerequisite for obtaining the type certification for an aircraft.
Shuang Lv
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Discussions on some problems of full-scale aircraft fatigue test
Hangkong gongcheng jinzhanFull-scale aircraft fatigue test is a large, complex and long-lasting ground verification test required by the specification to sustain aircraft structural integrity program and meet airworthiness requirements.
ZHANG Lixin
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Research Development on Bonded-bolted Hybrid Joint in Composite Structure
Hangkong gongcheng jinzhan, 2021 The composite bonded-bolted hybrid joint (BBHJ) is widely focused and developed in aerospace and aviation fields for its full consideration of advantages of bolt and bonded joint.
ZOU Peng +3 more
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Application research on 5G technology in fatigue test of full-scale aircraft
Hangkong gongcheng jinzhan, 2023 With the development of aircraft demand, and emerging of new material and new process, the test and validation technology of aircraft structure strength will also face new challenges.
LIU Bing, ZHANG Jianfeng, MU Bin
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Post-buckling analysis method of stiffened composite panels and test verification
Journal of Aeronautical Materials, 2021 Post-buckling analysis methods of fiber-reinforced T section stiffened composite panels were investigated. In this paper, the Finite Element Model was presented.
LIN Guowei, LI Xinxiang
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Nonlinear Modal Analysis of a Full-Scale Aircraft [PDF]
Journal of Aircraft, 2013 Nonlinear normal modes, which are defined as a nonlinear extension of the concept of linear normal modes, are a rigorous tool for nonlinear modal analysis. The objective of this paper is to demonstrate that the computation of nonlinear normal modes and of their oscillation frequencies can now be achieved for complex, real-world aerospace structures ...
Kerschen, Gaëtan +3 more
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Hangkong gongcheng jinzhan, 2022 Some problems such as large number of grids,high calculation cost,large proportion of memory and slow calculation efficiency may be encountered when calculating the dynamic characteristics of full-scale aircraft structures.
LI Peng, WANG Yahui
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Multi-joint and Large Load Wing Load Processing Method
Hangkong gongcheng jinzhan, 2020 For test piece lacking the right outer wing portion, the many and complicated butt joints, and the large test load, will bring great difficulty to the application of the wing load. Therefore the independent loading clamp is designed for the three sets of
WANG Xintao, XIA Long, LIU Xingke
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Advances in Mechanical Engineering, 2021 Interference-fit is attracting increasing attention in the aerospace field because of its excellent enhancement of the sealing and fatigue life of carbon fiber reinforced plastic (CFRP).
Jian Li +4 more
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Aircraft Position Prediction during the Crosswind Approach
Communications, 2022 Testing the impact of the drag coefficient on an F16 aircraft model, depending on the angle of attack was performed. First, a navigation model was introduced describing the preliminary and computational assumptions of the model.
Marek Grzegorzewski, Jerzy Biały
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