机构

• 长春光学精密机械与物... [5]
• 近代物理研究所 [5]
• 国家空间科学中心 [4]
• 理论物理研究所 [1]
• 沈阳自动化研究所 [1]

采集方式

• OAI收割 [16]

内容类型

• 会议论文 [8]
• 期刊论文 [8]

发表日期

• 2021 [1]
• 2020 [1]
• 2017 [2]
• 2016 [3]
• 2015 [2]
• 2011 [1]
• 更多

学科主题

• Physics [1]
• 微波遥感 [1]

筛选

浏览/检索结果: 共16条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择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作者升序作者降序 Measurement of leakage neutron spectra for aluminium with D-T fusion neutrons and validation of evaluated nuclear data 期刊论文  OAI收割 FUSION ENGINEERING AND DESIGN, 2021, 卷号: 171, 页码: 6 作者:  Zhang, S.;  Niu, D.;  Wang, D. X.;  Nie, Y.;  Song, N.   |  收藏  |  浏览/下载：45/0  |  提交时间：2021/12/08 Aluminium  Integral benchmark experiment  Time-of-flight method  Evaluated nuclear data   Benchmark experiments with slab sample using time-of-flight technique at CIAE 期刊论文  OAI收割 ANNALS OF NUCLEAR ENERGY, 2020, 卷号: 136, 页码: 21 作者:  Nie, Yangbo;  Ren, Jie;  Ruan, Xichao;  Ding, Yanyan;  Zhang, Kai   |  收藏  |  浏览/下载：37/0  |  提交时间：2022/01/19 Benchmark experiment  Evaluated nuclear data  Neutron leakage spectrum  Time-of-flight technique  D-T neutron source  MCNP-4C  C/E value   Recent progress in nuclear data measurement for ADS at IMP 期刊论文  OAI收割 NUCLEAR SCIENCE AND TECHNIQUES, 2017, 卷号: 28, 页码: 10 作者:  Chen, Zhi-Qiang   |  收藏  |  浏览/下载：40/0  |  提交时间：2018/05/31 Accelerator-driven systems  Nuclear data measurement  Neutron Time-of-Flight spectrometer  Integral experiment  Evaluated nuclear data   Benchmarking of JEFF-3.2, FENDL-3.0 and TENDL-2014 evaluated data for tungsten with 14.8 MeV neutrons 期刊论文  OAI收割 NUCLEAR SCIENCE AND TECHNIQUES, 2017, 卷号: 28, 页码: 6 作者:  Zhang, Suyalatu;  Nie, Yang-Bo;  Ren, Jie;  Luo, Fei;  Ruan, Xi-Chao   |  收藏  |  浏览/下载：32/0  |  提交时间：2018/05/31 Integral experiment  D-T neutron source  Time-of-flight technique  Leakage neutron spectrum  Monte Carlo simulation  Evaluated nuclear data   The benchmark experiment on slab beryllium with D-T neutrons for validation of evaluated nuclear data 期刊论文  OAI收割 FUSION ENGINEERING AND DESIGN, 2016, 卷号: 105, 页码: 8-14 作者:  Ding, Y.;  Nie, Y.;  Liu, P.;  Zhou, Z.;  Ruan, X.   |  收藏  |  浏览/下载：27/0  |  提交时间：2018/05/31 Beryllium  Evaluated nuclear data  Benchmark experiment  Neutron leakage spectrum  Time-of-flight method  MCNP-4B   Height Precision of SAR Altimeter and Conventional Radar Altimeter Based on Flight Experimental Data 期刊论文  OAI收割 IEEE JOURNAL OF SELECTED TOPICS IN APPLIED EARTH OBSERVATIONS AND REMOTE SENSING, 2016, 卷号: 9, 期号: 6, 页码: 2676-2686 作者:  Shi, Lingwei;  Xu, Ke;  Liu, Peng;  Yang, Shuangbao;  Wang, Lei 收藏  |  浏览/下载：34/0  |  提交时间：2016/11/08 Airborne flight experiment  conventional radar altimeter (CRA)  height precision  SARAL   Height Precision of SAR Altimeter and Conventional Radar Altimeter Based on Flight Experimental Data 会议论文  OAI收割 IEEE International Geoscience and Remote Sensing Symposium (IGARSS), Milan, ITALY, JUL 26-31, 2015 作者:  Shi, Lingwei;  Xu, Ke;  Liu, Peng;  Yang, Shuangbao;  Wang, Lei 收藏  |  浏览/下载：51/0  |  提交时间：2016/11/08 Airborne flight experiment  conventional radar altimeter (CRA)  height precision  SARAL   Experimental Investigation for RUAV's Actuator Fault Detections with AESMF 期刊论文  OAI收割 INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS, 2015, 卷号: 12, 页码: 1-13 作者:  Song DL(宋大雷);  Qi JT(齐俊桐);  Yang LY(杨丽英);  Han JD(韩建达) 收藏  |  浏览/下载：38/0  |  提交时间：2015/08/24 RUAV  actuator fault detection  AESMF  flight experiment investigation   THE ALTIMETER PRECISION COMPARISON BETWEEN SAR MODE AND CONVENTIONAL MODE THROUGH AIRBORNE EXPERIMENT 会议论文  OAI收割 IEEE International Geoscience and Remote Sensing Symposium (IGARSS), Milan, ITALY, JUL 26-31, 2015 作者:  Xu, Ke;  Liu, Peng;  Shi, Lingwei;  Wang, Lei;  Yu, Xiufen 收藏  |  浏览/下载：43/0  |  提交时间：2016/04/22 SARAL  CRA  height precision  airborne flight experiment   A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文  OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏  |  浏览/下载：71/0  |  提交时间：2013/03/25 In this paper  a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime  but not accurate enough in the supersonic regime. 2011 IEEE.