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浏览/检索结果: 共12条，第1-10条 帮助 限定条件 发表日期：2016    专题：北京航空航天大学    第一署名单位    第一作者单位    通讯作者单位     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择作者升序作者降序题名升序题名降序发表日期升序发表日期降序提交时间升序提交时间降序 Online Fault-Tolerant Onboard Aeroengine Model Tuning Structure 期刊论文 International Journal of Aerospace Engineering, 2016, 卷号: 2016 作者:  Ding, Shuiting;  Yuan, Ye;  Xue, Naiyu;  Liu, Xiaofeng 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 Aircraft engines  Health  Switching systems  Aeroengine model  Channel switching  Fault diagnostics  Fault tolerant control  Health degradation  Health management  Tuning structure  Working process  Fault tolerance   Multidisciplinary design optimization research of overall aero-engine based on flow path 会议论文 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference 作者:  Shen, X.;  Hu, W. 收藏  |  浏览/下载：2/0  |  提交时间：2019/12/30 Aerodynamics  Design  Design aids  Efficiency  Engines  Machine design  Aero-dynamic performance  High pressure compressor  Maximum Efficiency  Multi-disciplinary designs  Multi-disciplinary optimizations  Multidisciplinary design optimization  Potential capability  Structural strength  Aircraft engines   Adaptive Sliding-Mode Observer Design for a Selective Catalytic Reduction System of Ground-Vehicle Diesel Engines 期刊论文 IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2016, 卷号: 21, 页码: 2027-2038 作者:  Zhang, Hui;  Wang, Junmin 收藏  |  浏览/下载：2/0  |  提交时间：2019/12/30 Adaptive sliding-mode observer  diesel engine  observer design  selective catalytic reduction   Characteristics of pressure wave in common rail fuel injection system of high-speed direct injection diesel engines 期刊论文 ADVANCES IN MECHANICAL ENGINEERING, 2016, 卷号: 8 作者:  Herfatmanesh, Mohammad Reza;  Peng, Zhijun;  Ihracska, Alexis;  Lin, Yuzhen;  Lu, Lipeng 收藏  |  浏览/下载：5/0  |  提交时间：2019/12/30 Diesel engine  common rail fuel injection  high pressure  pressure wave  multiple injections   An Integrated Optimization Design Method Based on Surrogate Modeling Applied to Diverging Duct Design 期刊论文 INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 卷号: 33, 页码: 395-405 作者:  Lu Hanan;  Li Qiushi;  Li Shaobin 收藏  |  浏览/下载：4/0  |  提交时间：2019/12/30 uniform design  response surface methodology  genetic algorithm  diverging duct  optimization design   Numerical Study of the Effect of Secondary Vortex on Three-Dimensional Corner Separation in a Compressor Cascade 期刊论文 INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 卷号: 33, 页码: 9-18 作者:  Liu, Yangwei;  Yan, Hao;  Lu, Lipeng 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/30 cascade  corner separation  secondary flow  vortex   Study of the Standard k-epsilon Model for Tip Leakage Flow in an Axial Compressor Rotor 期刊论文 INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 卷号: 33, 页码: 353-360 作者:  Gao, Yanfei;  Liu, Yangwei;  Zhong, Luyang;  Hou, Jiexuan;  Lu, Lipeng 收藏  |  浏览/下载：6/0  |  提交时间：2019/12/30 standard k-epsilon model  turbulence anisotropy  non-equilibrium  tip leakage flow   Aerodynamic Design and Numerical Analysis of Supersonic Turbine for Turbo Pump 期刊论文 INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2016, 卷号: 33, 页码: 239-252 作者:  Fu, Chao;  Zou, Zhengping;  Kong, Qingguo;  Cheng, Honggui;  Zhang, Weihao 收藏  |  浏览/下载：3/0  |  提交时间：2019/12/30 supersonic turbine  velocity diagram  nozzle shockwave  unsteady flow   DocChat: An information retrieval approach for chatbot engines using unstructured documents 会议论文 54th Annual Meeting of the Association for Computational Linguistics, ACL 2016, Berlin, Germany, 2016-08-07 作者:  Yan, Zhao;  Duan, Nan;  Bao, Junwei;  Chen, Peng;  Zhou, Ming 收藏  |  浏览/下载：2/0  |  提交时间：2019/12/30 Partition method for improvement of piecewise linear model with full envelope covered 期刊论文 Hangkong Dongli Xuebao/Journal of Aerospace Power, 2016, 卷号: 31, 页码: 3042-3053 作者:  Yang, S.-B.;  Wang, X.;  Long, Y.-F.;  Li, Z.-P.;  Hu, Z.-Z. 收藏  |  浏览/下载：6/0  |  提交时间：2019/12/30 Aerodynamics  Flight simulators  Mach number  Nonlinear systems  Partitions (building)  Piecewise linear techniques  Sea level  Turbofan engines  Ambient conditions  Corrected parameters  Full envelope  Operating condition  Piecewise linear modeling  Real time requirement  Standard conditions  Static conditions  Flight envelopes