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Motion error based robust topology optimization for compliant mechanisms under material dispersion and uncertain forces 期刊论文
STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, 2018, 卷号: 57, 期号: 6, 页码: 2161-2175
作者:  Wang XJ;  Geng XY;  Wang L;  Wang RX(王睿星);  Shi QH
收藏  |  浏览/下载:33/0  |  提交时间:2018/07/17
Compliant Mechanisms  Uncertainties  Motion Accuracy  Robust Design  Topology Optimization  
Strain-Limiting Substrates Based on Nonbuckling, Prestrain-Free Mechanics for Robust Stretchable Electronics 期刊论文
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2017, 卷号: 84, 期号: 12, 页码: 121010
作者:  Zhang MY;  Liu H;  Cao P;  Chen B;  Hu JQ(胡剑桥);  Chen YL;  Pan B;  Fan JA;  Li R;  Zhang LJ;  Su YW(苏业旺)
浏览  |  Adobe PDF(4302Kb)  |  收藏  |  浏览/下载:89/15  |  提交时间:2017/12/18
Strain-limiting Substrates  Nonbuckling  Prestrain-free Design  Stretchable Electronics  
The Exploration of Superiority about the Non-probability Reliability-Based Design Optimization Compared to the Safety Factor Method 会议论文
2ND INTERNATIONAL CONFERENCE ON APPLIED MECHANICS, ELECTRONICS AND MECHATRONICS ENGINEERING (AMEME), Beijing, PEOPLES R CHINA, OCT 22-23, 2017
作者:  Fan WC;  Wang XJ;  Wang RX(王睿星);  Wang L
浏览  |  Adobe PDF(1122Kb)  |  收藏  |  浏览/下载:928/9  |  提交时间:2018/06/06
Superiority Exploration  Mathematical Proof  Non-probability Reliability-based Design Optimization  Safety Factor Method  
高压捕获翼位置设计方法研究 期刊论文
力学学报, 2016, 卷号: 48, 期号: 3, 页码: 576-584
作者:  李广利;  崔凯;  肖尧;  徐应洲
浏览  |  Adobe PDF(992Kb)  |  收藏  |  浏览/下载:90/11  |  提交时间:2016/12/16
High-speed Vehicles  High Pressure Capturing Wing  Uniform Experimental Design  Polynomial Surrogate Model  
基于实验设计方法的高超声速飞机前缘型线优化分析 期刊论文
力学学报, 2016, 卷号: 48, 期号: 2, 页码: 290-299
作者:  胡守超;  崔凯;  李广利;  肖尧;  司徒明
浏览  |  Adobe PDF(1239Kb)  |  收藏  |  浏览/下载:69/7  |  提交时间:2016/12/16
Hypersonic Airplane  Air-breathing Vehicle  Shape Optimization  Parameterization  Uniform Design  
高速列车头型气动反设计方法 期刊论文
浙江大学学报. 工学版, 2016, 卷号: 50, 期号: 4, 页码: 631
作者:  陈大伟;  姚拴宝;  刘韶庆;  郭迪龙
浏览  |  Adobe PDF(2962Kb)  |  收藏  |  浏览/下载:79/21  |  提交时间:2016/12/16
Inverse Design  Support Vector Regression(Svr)  Multi-objective Design  High-speed Train  
Parametric design and optimization of high speed train nose 期刊论文
OPTIMIZATION AND ENGINEERING, 2016, 卷号: 17, 期号: 3, 页码: 605-630
作者:  Yao SB(姚拴宝);  Guo DL(郭迪龙);  Sun ZX(孙振旭);  Chen DW(陈大伟);  Yang GW(杨国伟);  Sun, ZX (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Applicat Mech Engn Syst, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2807Kb)  |  收藏  |  浏览/下载:81/19  |  提交时间:2016/12/08
Parametric Design  Aerodynamic Shape  Svm Model  Pso  Multi-objective Optimization  High Speed Trains  
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
作者:  Xiao YB(肖雅斌);  Yue LJ(岳连捷);  Ma SH;  Zhang XY(张新宇);  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
浏览  |  Adobe PDF(1353Kb)  |  收藏  |  浏览/下载:52/8  |  提交时间:2016/09/14
Hypersonic Inlet  Shape Transition  Inward Turning  Scramjet  Design Method  
Splitting of the neutral mechanical plane depends on the length of the multi-layer structure of flexible electronics 期刊论文
PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2016, 卷号: 472, 期号: 2190, 页码: 20160087
作者:  Li S;  Su YW(苏业旺);  Li R;  Su, YW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.;  Su, YW (reprint author), Northwestern Univ, Dept Civil & Environm Engn, Evanston, IL 60208 USA.;  Su, YW (reprint author), Northwestern Univ, Dept Mech Engn, Evanston, IL 60208 USA.;  Li, R (reprint author), Dalian Univ Technol, Dept Engn Mech, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China.
浏览  |  Adobe PDF(1271Kb)  |  收藏  |  浏览/下载:67/6  |  提交时间:2016/09/14
Neutral Mechanical Plane  Multi-layer Structure  Flexible Electronics  Structure Design  
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Cui K(崔凯);  Hu SC(胡守超);  Li GL;  Xiao Y(肖尧);  Situ M
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载:70/34  |  提交时间:2017/05/05
Aero  Dynamic Performance  Aerodynamic Performance Predictions  Design Methodology  Flight Altitudes  Numerical Results  Propulsion System  Turbulent Models  Wing Body Aircraft