Test Research on Fuselage Panel Subjected to Internal Pressure Load by Zang Weifeng, Chen An, Dong Dengke

Subjects: “…fuselage panel…”
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Analysis of Metallic Fuselage Frame Pitch and Cross Section Parameters by Ma Jun

Subjects: “…metallic fuselage…”
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SIMULATION ANALYSIS OF CARGO LOADING ON CRASHWORTHINESS OF COMPOSITE FUSELAGE SECTION by XIE Jiang, MOU HaoLei, ZOU TianChun, FENG ZhenYu, MAO KeYi

Subjects: “…Composite fuselage section;Crashworthiness;Cargo loading;Acceleration response;Energy-absorbing characteristics…”
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RESEARCH ON TEST METHOD OF FUSELAGE PANEL SUBJECTED TO SHEAR LOAD by ZANG WeiFeng, SU ShaoPu, ZHANG HaiYing, DONG DengKe

Subjects: “…Fuselage panel;Shear load;Boundary condition simulation;"D"jig;Arch angle connector;Shear stress…”
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DAMAGE TOLERANCE EXPERIMENT AND ANALYSIS OF STIFFENED FUSELAGE PANEL WITH LONGITUDINAL CRACK by CHEN An, WEI YuLong, LIAO JiangHai, DONG DengKe

Subjects: “…Fuselage panel;Longitudinal crack;Damage tolerance experiment;Crack propagation;Residual strength;Stress intensify factor…”
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Analysis of Rotor/Propeller/Fuselage Interaction Characteristics of High-speed Helicopter by SHEN Suiyuan, ZHU Qinghua, ZHU Zhenhua, ZENG Jianan, CHEN Jianwei

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RESEARCH ON TEST METHOD OF FUSELAGE PANEL SUBJECTED TO INTERNAL PRESSURE LOAD by ZANG WeiFeng, DONG DengKe, ZHANG HaiYing

“…The test method of fuselage panel subjected to internal pressure load is an important technique for aircraft structure strength research.The constraint simulation technique for the curved and straight boundaries of fuselage panel was studied based on boundary requirements.A test method using "D"jig to simulate the straight boundary conditions and airproof end-plate to simulate the curved boundary conditions of fuselage panels were proposed.A test panel and a set of fixtures were designed and manufactured,and validation tests were conducted.Measured stresses in test are reasonably distributed and are consistent with theoretic result.The proposed test method is proven to be proper and valid,and it provides reference for configuration-selection tests of fuselage panel subjected to internal pressure load.…”
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Analysis on Trap Panel Structure for Aircraft Outer Wing-fuselage Connection by Tang Ping, Liu Ting, Zhang Mingxing

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Reliability analysis of composite sandwich structure for fuselage skin based on surrogate model by DING Zhendong, LI Hongshuang, GUAN Xiaole

“…In order to reduce the computational effort, the Kriging surrogate models of failure modes were constructed, and the subset simulation method was used to predict the system failure probability of the sandwich structure of fuselage skin. The proposed computational framework provides support and tool for the fine design of composite sandwich structure.…”
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Fracture damage of integrated composite joint for fuselage structure under tensile loading

“…In order to solve the complex load transfer and structural design of the joint structures including skin, longeron and frame in the composite fuselage, the adhesively bonded integrated composite joint was designed. …”
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Research and strength analysis of hoop bending test of composite fuselage integral frame by LIANG Heng, TANG Guowei, ZHENG Xiaoling

Subjects: “…fuselage frame…”
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Study on the Effects of Rear Fuselage Contraction Patterns on Aerodynamic Characteristics of a General Aviation Airplane by WANG Xiaolu, LIU Weiwei, XU Xiangbo, ZHU Shunshun

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EXPERIMENT AND SIMULATION RESEARCH ON UNIFORM SUPERCHARGED FATIGUE CRACK INITIATION OF AIRCRAFT FUSELAGE SKIN by LIU LiPing, ZHANG Fang, ZHONG XiaoKun, BAO Rui, XU JianXin, QIN WenChao

Subjects: “…Fuselage skin;Uniform supercharged;Fatigue crack;Initiation…”
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ANALYSIS AND EVALUATION FUSELAGE SECTION’S CRASHWORTHINESS OF TYPICAL CIVIL AIRPLANE BASED ON PASSENGER RESPONSE by ZHU XianFei, FENG YunWen, XUE XiaoFeng, ZHU ZhengZheng

Subjects: “…Fuselage section structure;Dummy-seat-restraint system;Crashworthiness analysis;Crashworthiness evaluation;Numerical simulation…”
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Research on Compression Buckling and Failure Characteristics of Composite Fuselage Cap-stringer Stiffened Panel by LI Zhen, CHENG Liping

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Balancing load design for full-size static strength test of civil aircraft in front fuselage serious condition by YUAN Qiangfei

“…For the thin-wall structure, the balancing in non-assessment area has great influence on assess-ment area. Taking a front fuselage serious condition of a certain civil aircraft as an example, the balancing load scheme of full-size static strength test is studied based on the finite element model. …”
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Research on Calculation Method for Acoustic Scattering of Helicopter Noise

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Research of Design Technology of Large Opening Lifting Photo-electric Pod by MIAO Zhitao, LI Jianping, BAI Yanjie

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A Method for Calculating Angle of Attack and Sideslip Angle by WEN Qing

“…The wind tunnel test is carried out on the front fuselage model of a large amphibious aircraft,according to the characteristics of the angle of attack sensors on both sides of the fuselage affected by the sideslip angle. …”
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Research on the cantilever roadheader positioning based on near-infrared binocular stereo vision by WANG Xue, ZHOU Hongxu, ZHANG Lei, WANG Huaying

“…The three-dimensional spatial positioning of the roadheader fuselage and the cutting part is realized through image processing and pose calculation. …”
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