云南高校图书馆联盟文献共享服务平台- FUSELAGE

FUSELAGE: 作品数：30被引量：61H指数：4; 导出分析报告; 相关领域：航空宇航科学技术更多>>; 相关作者：高正红黄江涛赵轲白俊强郭亮更多>>; 相关机构：南京航空航天大学西北工业大学中国飞机强度研究所意柯那(上海)工业设计有限公司更多>>; 相关期刊：《International Journal of Modeling, Simulation, and Scientific Computing》《China's Foreign Trade》《Beijing Review》《Science China(Physics,Mechanics & Astronomy)》更多>>; 相关基金：国家自然科学基金中国航空科学基金更多>>

Development of a crawler chassis attitude adjustment device for a selfpropelled maize harvester and experiment of fuselage leveling: 《International Journal of Agricultural and Biological Engineering》2024年第6期111-120,共10页Hewen Tan Gang Wang Shuhui Zhou Honglei Jia Zhaobo Zou Minghao Qu; financially supported by the National Key R&D Program of China(Grant No.2022YFD1500701);the Jilin Science and Technology Development Plan(Grant Nos.20210202019NC,20220203081SF).; Self-propelled maize harvesters are prone to overturning when operating on sloping ground.Solving this problem presents a major technical challenge for researchers.Existing undercarriage leveling technologies are most...; 关键词：crawler harvesters adjustment mechanism leveling control systems vectors method

Collaborative force and shape control for large composite fuselage panels assembly被引量：2: 《Chinese Journal of Aeronautics》2023年第7期213-225,共13页Zhanghao WANG Dongsheng LI Liheng SHEN Yi SUI Yunong ZHAI; supported by National Natural Science Foundation of China(No.52105502);Fund of National Engineering and Research Center for Commercial Aircraft Manufacturing(Nos.COMAC-SFGS-2019-263 and COMAC-SFGS-2019-3731);the Fundamental Research Funds for the Central Universities(No.3042021601).; This study proposed a force and shape collaborative control method that combined method of influence coefficients(MIC)and the elitist nondominated sorting genetic algorithm(NSGA-II)to reduce the shape deviation caused...; 关键词：ASSEMBLY Collaborative force and shape control Composite panel Hexapod parallel robots Method of influence coefficients

A Realistic 3D Non-Stationary Channel Model for UAV-to-Vehicle Communications Incorporating Fuselage Posture被引量：1: 《China Communications》2023年第6期277-290,共14页Boyu Hua Tongtong Zhou Qiuming Zhu Kai Mao Junwei Bao Weizhi Zhong; supported by the National Natural Science Foundation of China,No.62271250;the National Key Scientific Instrument and Equipment Development Project,No.61827801;Key Technologies R&D Program of Jiangsu(Prospective and Key Technologies for Industry),No.BE2022067,BE2022067-1 and BE2022067-3;the Natural Science Foundation of Jiangsu Province,No.BK20211182;the open research fund of National Mobile Communications Research Laboratory,Southeast University,No.2022D04;the Experimental technology research and development,No.SYJS202304Z。; Considering the unmanned aerial vehicle(UAV) three-dimensional(3D) posture, a novel 3D non-stationary geometry-based stochastic model(GBSM) is proposed for multiple-input multipleoutput(MIMO) UAV-to-vehicle(U2V) chann...; 关键词：channel model unmanned aerial vehicle NON-STATIONARY fuselage posture

Impact of Crash Environments on Crashworthiness of Fuselage Section被引量：2: 《Transactions of Nanjing University of Aeronautics and Astronautics》2022年第S01期1-8,共8页TANG Huan ZHU Shuhua LIU Xiaochuan XI Xulong; supported by the Special Research on Civil Aircraft(No.MJ-2017-F15); In order to study the crash resistance of the civil aircraft structure in different crash environments,two environmental models of soft soil and water are established to analyze the dynamic response of the fuselage se...; 关键词：CRASHWORTHINESS dynamic response fuselage section soft soil WATER

WORLD: 《Beijing Review》2019年第20期8-9,共2页; RUSSIA The burnt fuselage of an Aeroflot SSJ-100 passenger plane is seen on the tarmac at Sheremetyevo International Airport in Moscow on May 6. Forty-one deaths were reported after the plane caught fire before making...; 关键词：RUSSIA The burnt FUSELAGE PASSENGER PLANE EMERGENCY LANDING

A New Spot Welding Technique for Fuselage: 《材料导报》2019年第10期1595-1596,共2页CHEN Dan CHAI Peng ZHAO Huaxia XIONG Jiangtao LI Jinglong; High strength aluminum alloys(series 2XXX and 7XXX)are kinds of precipitation-hardening alloys,which have been widely applied in manufacturing of fuselage for their high strength-to-weight ratio,good fatigue performan...; 关键词：HIGH STRENGTH ALUMINUM ALLOYS kinds

A model-based prognostics method for fatigue crack growth in fuselage panels被引量：3: 《Chinese Journal of Aeronautics》2019年第2期396-408,共13页Yiwei WANG Christian GOGU Nicolas BINAUD Christian BES Jian FU; partially funded by the National Natural Science Foundation of China (No.51805262); This paper proposes a model-based prognostics method that couples the Extended Kalman Filter(EKF) and a new developed linearization method. The proposed prognostics method is developed in the context of fatigue crack ...; 关键词：Aircraft FUSELAGE PANELS Extended Kalman filter Fatigue crack propagation LINEARIZATION METHOD MODEL-BASED PROGNOSTICS

Effect of repair methods on mechanical behaviors of repair area in composite laminate fuselage skin with different damage size: 《Materials Science(Advanced Composite Materials)》2018年第3期15-42,共28页Liping Liu Yucan Wang Jing Tian Ruifeng Wang Jianxin Xu; This project obtained designated funds from National Natural Science Foundation (No. 51405491, No. 51605331);Basic Scientific Research Foundation of Central University (No. 3122017028).; Composite laminates are widely used in the large civil aircrafts because of their excellent mechanical properties. The maintenance and repair of composite laminates become essential. In this paper, a new adhesive-rive...; 关键词：stress distribution ADHESIVE REPAIR adhesive-rivet hybrid REPAIR composite LAMINATE FUSELAGE SKIN

A model for real-time computation of fuselage-rotor interference: 《International Journal of Modeling, Simulation, and Scientific Computing》2017年第4期10-24,共15页Berend G.van der Wall Jianping Yin; A simple analytical real-time capable model to account for fuselage-induced velocities at rotor blade elements is described at the example of the Bo105 fuselage.Data of the fuselage-induced flow fields in the volume o...; 关键词：Helicopter aerodynamics fuselage-rotor interference real-time simulation

Developing an engineering-statistical model for estimating aerodynamic coefficients of helicopter fuselage: 《Chinese Journal of Aeronautics》2017年第1期175-185,共11页Hossein Sheikhi Abas Saghaie; The design of the geometric shape of a helicopter fuselage poses a serious challenge for designers. The most important parameter in determining the shape of the helicopter fuselage is its aerodynamic coefficients. The...; 关键词：Aerodynamic coefficients Computaticnal fluid dynamics （CFD） Engineering-statistical model Helicopter fuselage Wind tunnel test

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