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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Bird Strikes and Aircraft Fuselage Color: A Correlational Study by Esteban Fernández-Juricic, Jim Gaffney, Bradley F. Blackwell, Patrice Baumhardt

“…We estimated the bird-strike rates and compared them among airline companies using different fuselage color schemes, while controlling for aircraft type. …”
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Material Selection for Fuselage Using Integrated SWARA-MULTIMOORA Approach by Aslı ÇALIŞ BOYACI, Mehmet Çağrı TÜZEMEN

Subjects: “…fuselage…”
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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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Mechanical and Metallurgical behaviour of Aluminum/graphene nanocomposites in Fuselage applications by Tarun Kumar Kotteda, Manoj Kumar, Pramod Kumar, Ajay Gupta, Sita Rama Raju Kalidindi

“…Use of high specific strength materials for such fuselage structure greatly reduces the emissions generated by air vehicles. …”
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Experimental and numerical investigations on the aerodynamics of a simplified helicopter fuselage by Cheawchan, Atcha-uea

“…Depending on helicopter weight class, fuselage parasite drag contributes up to 70 percent of total helicopter drag. …”
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New metal fuselage section arrangement minimize assembly time by Hassan, Mohamed P., Mohd Rafie, Azmin Shakrine

“…Analyzing innovation attempts from 1950s to present showed the introduction of the coil fuselage concept and how it developed into the integral frames and panels concept currently pursued. …”
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Crash Simulation Of A Composite Unmanned Aerial Vehicle Fuselage by Yidris, Noorfaizal

“…The simulation of the composite fuselage sections was carried out, refined several times and validated with the experimental results. …”
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Drag study of variety rear upsweep of helicopter fuselage [electronic resource] / by 327023 Mohamed Mirzan Mohamed Mustafa, Fakulti Kejuruteraan Mekanikal

Experimental and numerical simulation of the wall-pressure fluctuation on the isolated helicopter fuselage by Batrakov Andrei

“…The object of investigation was an isolated helicopter fuselage. Investigation was carried out by experimental and numerical methods. …”
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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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Structural Health Monitoring Cost Estimation of a Piezosensorized Aircraft Fuselage by Ilias N. Giannakeas, Zahra Sharif Khodaei, M. H. Ferri Aliabadi

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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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Impact localization on a composite fuselage with a sparse network of accelerometers by Goutaudier, Dimitri, Osmond, Guillaume, Gendre, Didier

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Structural optimization of composite fuselage panel including buckling and manufacturing constraints by Tanut Ungwattanapanit.

“…Multidisciplinary Design Optimization (MDO) techniques were successfully developed and applied in sizing a composite fuselage panel of narrow-body airliner. The detailed finite element fuselage panel was undergone optimization process developed around gradient-based optimizer MSC Nastran SOL 200. …”
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PEMANFAATAN LIMBAH TANDAN KOSONG SAWIT (TKS) SEBAGAI MATERIAL ALTERNATIF DALAM PEMBUATAN BADAN WAHANA TERBANG TIPE FIXED WING ATHA MAPPER 2150 by Kaspul Anuar, Warman Fatra, Anita susilawati

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A computational simulation of rotor - fuselage flow interaction in hovering and forward flight / by 284422 Mohamad Hafiz Ismail, Abas Ab. Wahab

Wind tunnel testing of a helicopter with different fuselage rear upsweep angle / by 308489 Azrul Ahmad, Wan Zaidi Wan Omar, supervisor, Fakulti Kejuruteraan Mekanikal