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浏览/检索结果: 共9条，第1-9条 帮助 限定条件 发表日期：2020     已选(0)清除 条数/页：5101520253035404550556065707580859095100   排序方式：请选择发表日期升序发表日期降序提交时间升序提交时间降序题名升序题名降序作者升序作者降序 Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来) 收藏  |  浏览/下载：22/0  |  提交时间：2021/03/30 High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique   Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach 期刊论文 IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2020, 卷号: 31, 期号: 11, 页码: 5005-5013 作者:  Chai, Runqi;  Tsourdos, Antonios;  Savvaris, Al;  Chai, Senchun;  Xia, Yuanqing 收藏  |  浏览/下载：15/0  |  提交时间：2021/01/06 Attitude control  Real-time systems  Trajectory optimization  Trajectory planning  Attitude control  bilevel structure  deep neural network (DNN)  six-degree-of-freedom (6-DOF) hypersonic vehicle (HV)  trajectory planning   Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10 作者:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY 收藏  |  浏览/下载：40/0  |  提交时间：2020/11/30 Optimization design  Drag reduction  Supersonic flow  Energy deposition  Opposing jet   低导热超高温热障涂层的制备及其性能研究 学位论文 : 中国科学院大学, 2020 作者:  杨明 收藏  |  浏览/下载：21/0  |  提交时间：2021/09/07 热障涂层,热导率,热应力,热烧蚀   Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition 期刊论文 INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362 作者:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟) 收藏  |  浏览/下载：63/0  |  提交时间：2020/06/22 Coupled flow-thermal analysis  Thermal protection system  Basic direct correction method (BDCM)  Improved DCM (IDCM)  Iteration solution method (ISM)   Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文 ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310 作者:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY 收藏  |  浏览/下载：18/0  |  提交时间：2020/05/18 Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet   Coupling Model and Electronic Compensation of Antenna-Radome System for Hypersonic Vehicle With Effect of High-Temperature Ablation 期刊论文 IEEE TRANSACTIONS ON ANTENNAS AND PROPAGATION, 2020, 卷号: 68, 期号: 3, 页码: 2340-2355 作者:  Wang, Congsi;  Wang, Yan;  Chen, Yuankui;  Gao, Wei;  Xu, Qian 收藏  |  浏览/下载：28/0  |  提交时间：2020/06/28 Active phased array antenna  electronic compensation  high-temperature ablation  hypersonic vehicle  performance coupling   An Improvement of PWPF in Reaction Control System of Hypersonic Vehicle 会议论文 Chinese Intelligent Systems Conference, CISC 2019, Haikou, China, 2019-10-26 作者:  Song, Jia;  Bian, Likun 收藏  |  浏览/下载：29/0  |  提交时间：2019/12/30 Numerical study on aerodynamic performance of waverider with a new bluntness method 期刊论文 Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020 作者:  Qu ZP;  Xiao HD;  Lv MY;  Li GL(李广利);  Cui K(崔凯) 收藏  |  浏览/下载：7/0  |  提交时间：2021/06/11 bluntness method  computational fluid dynamics  hypersonic  volume  Waverider