AIRPLANE

作品数:64被引量:186H指数:8
导出分析报告
相关作者:刘润松石磊黄敏齐晶晶刘伟更多>>
相关机构:北京航空航天大学中国民用航空飞行学院中国直升机设计研究所中国北车集团北京二七轨道交通装备有限责任公司更多>>
相关期刊:更多>>
相关基金:国家自然科学基金中国博士后科学基金中国航空科学基金国家教育部博士点基金更多>>
-

检索结果分析

结果分析中...
选择条件:
  • 期刊=Chinese Journal of Aeronauticsx
条 记 录,以下是1-10
视图:
排序:
Prior-guided GAN-based interactive airplane engine damage image augmentation method被引量:2
《Chinese Journal of Aeronautics》2022年第10期222-232,共11页Rui HUANG Bokun DUAN Yuxiang ZHANG Wei FAN 
Natural Science Foundation of Tianjin,China(No.20JCQNJC00720)。
Deep learning-based methods have achieved remarkable success in object detection,but this success requires the availability of a large number of training images.Collecting sufficient training images is difficult in de...
关键词:Airplane engine Damage detection Data augmentation GAN INTERACTIVE 
Reliability and global sensitivity analysis for an airplane slat mechanism considering wear degradation被引量:2
《Chinese Journal of Aeronautics》2021年第1期163-170,共8页Changcong ZHOU Haodong ZHAO Qi CHANG Mengyao JI Chen LI 
supported by the National Natural Science Foundation of China(NSFC51975476);the Natural Science Basic Research Plan in Shaanxi Province(2020JM-135);Aerospace Science and Technology Foundation of China。
This paper focuses on the issue of reliability and global sensitivity analysis for an airplane slat mechanism considering the uncertainties in the wear process of mechanical components.First,the multi-body kinematic m...
关键词:Slat mechanism Roller wheel Wear degradation RELIABILITY Sensitivity 
A data-driven health indicator extraction method for aircraft air conditioning system health monitoring被引量:17
《Chinese Journal of Aeronautics》2019年第2期409-416,共8页Jianzhong SUN Chaoyi LI Cui LIU Ziwei GONG Ronghui WANG 
supported by the National Natural Science Foundation of China (61403198);the Jiangsu Province Natural Science Foundation of China (BK20140827);China Postdoctoral Science Foundation (2015M581792)
Prognostics and Health Management(PHM) has become a very important tool in modern commercial aircraft. Considering limited built-in sensing devices on the legacy aircraft model,one of the challenges for airborne syste...
关键词:Air conditioning SYSTEM Aircraft HEALTH MONITORING AIRPLANE condition MONITORING SYSTEM HEALTH INDICATOR PROGNOSTICS and HEALTH management 
Integrated optimization on aerodynamics-structure coupling and flight stability of a large airplane in preliminary design被引量:2
《Chinese Journal of Aeronautics》2018年第6期1258-1272,共15页Xiaozhe WANG Zhiqiang WAN Zhu LIU Chao YANG 
supported by the National Key Research and Development Program (No.2016YFB0200703);the Academic Excellence Foundation of Beihang University for Ph.D. Students
The preliminary phase is significant during the whole design process of a large airplane because of its enormous potential in enhancing the overall performance. However, classical sequential designs can hardly adapt t...
关键词:Aeroelasticity Integrated optimization Multidisciptinary analysis Large airplane Preliminary design 
Mass and performance optimization of an airplane wing leading edge structure against bird strike using Taguchi-based grey relational analysis被引量:7
《Chinese Journal of Aeronautics》2016年第4期934-944,共11页Hassan Pahange Mohammad Hossein Abolbashari 
Collisions between birds and aircraft are one of the most dangerous threats to flight safety. In this study, smoothed particles hydrodynamics(SPH) method is used for simulating the bird strike to an airplane wing lead...
关键词:Bird strike Grey relational analysis Multi-objective optimization Smooth particle hydrody namics(SPH) Wing leading edge structure 
Drop test and crash simulation of a civil airplane fuselage section被引量:15
《Chinese Journal of Aeronautics》2015年第2期447-456,共10页Liu Xiaochuan Guo Jun Bai Chunyu Sun Xiasheng Mou Rangke 
supported by the Ministry Level Project of China
Crashworthiness of a civil airplane fuselage section was studied in this paper. Firstly, the failure criterion of a rivet was studied by test, showing that the ultimate tension and shear failure loads were obviously a...
关键词:Civil airplane Drop test Finite element method Fuselage section Rivet failure 
Effect of pitch angle on initial stage of a transport airplane ditching被引量:22
《Chinese Journal of Aeronautics》2013年第1期17-26,共10页Guo Baodong Liu Peiqing Qu Qiulin Wang Jiawen 
co-supported by Aeronautical Science Foundation of China (No.20102351023);Research Fund for the Doctoral Program of Higher Education of China (No. 20091102120021)
Airworthiness regulations require that the transport airplane should be proved to ensure the survivability of the ditching for the passengers. The planned ditching of a transport airplane on the calm water is numerica...
关键词:CRASHWORTHINESS Fluid structure interaction HYDRODYNAMICS Multiphase flow Transport aircraft Water landing 
Aerodynamic Modeling and Parameter Estimation from QAR Data of an Airplane Approaching a High-altitude Airport被引量:21
《Chinese Journal of Aeronautics》2012年第3期361-371,共11页WANG Qing WU Kaiyuan ZHANG Tianjiao KONG Yi'nan QIAN Weiqi 
National Natural Science Foundation of China(60832012)
Aerodynamic modeling and parameter estimation from quick accesses recorder (QAR) data is an important technical way to analyze the effects of highland weather conditions upon aerodynamic characteristics of airplane....
关键词:civil airplane aerodynamics QAR data aerodynamic modeling aerodynamic parameter estimation flight safety EKF-MBF method neural network 
Interactive Multi-objective Optimization Design for the Pylon Structure of an Airplane被引量:4
《Chinese Journal of Aeronautics》2007年第6期524-528,共5页An Weigang Li Weiji 
Foundation item: National Natural Science Foundation of China (10377015)
The pylon structure of an airplane is very complex, and its high-fidelity analysis is quite time-consuming. If posterior preference optimization algorithm is used to solve this problem, the huge time consumption will ...
关键词:pylon structure multi-objective optimization algorithm interactive algorithm multi-objective particle swarm optimization neural network 
THE STUDY OF AIRPORT TERRAIN EFFECTS ON AUTOLAND FOR ANY AIRPLANE
《Chinese Journal of Aeronautics》1994年第1期38-44,共7页
THESTUDYOFAIRPORTTERRAINEFFECTSONAUTOLANDFORANYAIRPLANEDr.SaiF.Lee(No804PerryAve,MontebelloCa90640(13)728-58...
检索报告 对象比较 聚类工具 使用帮助 返回顶部