Turnitin
降AI改写
早检测系统
早降重系统
Turnitin-UK版
万方检测-期刊版
维普编辑部版
Grammarly检测
Paperpass检测
checkpass检测
PaperYY检测
Aerodynamic design optimization by using a continuous adjoint method
This paper presents the fundamentals of a continuous adjoint method and the applications
of this method to the aerodynamic design optimization of both external and internal flows …
of this method to the aerodynamic design optimization of both external and internal flows …
Efficient aeroelastic design optimization based on the discrete adjoint method
Y Zuo, G Chen, Y Li, Z GAO - Transactions of the Japan Society for …, 2014 - jstage.jst.go.jp
An approach for the aerodynamic optimization design of elastic configurations is
implemented and tested. Aeroelastic analysis was carried out by combining an Euler …
implemented and tested. Aeroelastic analysis was carried out by combining an Euler …
一种高效的 CFD/CSD 耦合飞行器多学科优化设计方法
左英桃， 王晓鹏， 陈云， 陈刚， 高**红 - 航空动力学报, 2014 - jasp.com.cn
建立了一种基于CFD/CSD (computational fluid dynamics/computational structure dynamics)
耦合的多学科优化设计方法. 该方法采用结构有限元方程进行结构特性分析 …
耦合的多学科优化设计方法. 该方法采用结构有限元方程进行结构特性分析 …
静气动弹性模型高速风洞试验研究
杨贤文， 余立， 吕彬彬， 郭洪涛， 杨振华… - 空气动力学 …, 2015 - kqdlxxb.xml-journal.net
对采用复合材料玻璃纤维, 碳纤维加工的静气动弹性模型进行了高速风洞试验研究,
测试了模型的柔度矩阵, 气动力, 表面压力, 弯/扭应变信号及弯/扭变形, 为静气动弹性模型刚度 …
测试了模型的柔度矩阵, 气动力, 表面压力, 弯/扭应变信号及弯/扭变形, 为静气动弹性模型刚度 …
An efficient method for multidisciplinary design optimization of aircraft based on CFD/CSD coupling
ZUO Ying-tao, W **ao-peng, C Yun, C Gang… - 航空动力学报, 2014 - jasp.com.cn
A multidisciplinary design optimization method based on CFD/CSD (computational fluid
dynamics/computational structure dynamics) coupling was built. The structural performance …
dynamics/computational structure dynamics) coupling was built. The structural performance …
A Design Method for Twist Distribution along Wing Span
X Liu, P Cheng, Y Zhao - IOP Conference Series: Materials …, 2019 - iopscience.iop.org
A design method for wing jig shape twist is proposed. Target cruising aerodynamic loads are
applied to structure model, and the deformation converge gradually using predictor …
applied to structure model, and the deformation converge gradually using predictor …
[ALINTI][C] 三维机翼气动结构多学科优化方法
徐兆可， 夏健， 高宜胜 - 中文版, 2018 - jasp.com.cn
三维机翼气动结构多学科优化方法 主办:**航空学会 北京航空航天大学 微信公众号 网站二维码
首页 期刊介绍 编委会 投稿须知 期刊订阅 广告合作 常见问题 联系我们 English 首页 > 过刊浏览 …
首页 期刊介绍 编委会 投稿须知 期刊订阅 广告合作 常见问题 联系我们 English 首页 > 过刊浏览 …
[ALINTI][C] Theory and method of aircraft multidisciplinary design optimization: current status and future direction
[ALINTI][C] 飞行器多学科优化设计研究现状与展望
**忠华， 龙腾， 宋学官， 张科施 - 气动研究与实验, 2020
[ALINTI][C] Research on Static Aero-elastic Characteristics of Wing in High Speed Wind Tunnel
Y Bo, J **ang, M **gzhong, W Guoliang - Aerodynamic Research & Experiment, 2020