机构

• 过程工程研究所 [2]
• 长春光学精密机械与物... [1]
• 上海应用物理研究所 [1]

采集方式

• OAI收割 [4]

内容类型

• 会议论文 [2]
• 期刊论文 [2]

发表日期

• 2023 [1]
• 2019 [1]
• 2016 [1]
• 2011 [1]

学科主题

筛选

浏览/检索结果: 共4条，第1-4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 A deep learning approach using temporal-spatial data of computational fluid dynamics for fast property prediction of gas-solid fluidized bed 期刊论文  OAI收割 KOREAN JOURNAL OF CHEMICAL ENGINEERING, 2023, 卷号: 40, 期号: 1, 页码: 57-66 作者:  Qin, Pengfei;  Xia, Zhaojie;  Guo, Li   |  收藏  |  浏览/下载：0/0  |  提交时间：2023/05/19 Gas-solid Fluidized Bed  CFD Surrogate Model  Deep Learning  Multi-scale Convolutional Neural Network  Voidage Distribution Prediction   Bubble formation and evolution behavior from vertical wall orifice 期刊论文  OAI收割 NUCLEAR SCIENCE AND TECHNIQUES, 2019, 卷号: 30, 期号: 12, 页码: - 作者:  Ma, ZW   |  收藏  |  浏览/下载：156/0  |  提交时间：2020/10/16 FLUID-DYNAMICS CFD  LIQUID CROSS-FLOW  COLUMN  VOLUME  SIMULATIONS  DETACHMENT  PREDICTION  FORCES   3-D NUMERICAL SIMULATION OF THE VAPOR-LIQUID FLOW AT THE SHELL SIDE OF SHELL-AND-TUBE HEAT EXCHANGERS 会议论文  OAI收割 24th International Conference on Nuclear Engineering, Charlotte, NC, JUN 26-30, 2016 作者:  Xiao, Q 收藏  |  浏览/下载：48/0  |  提交时间：2017/07/12 BUBBLE-COLUMN  STEAM-GENERATOR  TURBULENCE MODELS  CFD PREDICTION  SECONDARY-SIDE  INTERNALS  BUNDLES  FORCES   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：72/0  |  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.