找回密码
 To register

QQ登录

只需一步,快速开始

扫一扫,访问微社区

Titlebook: AeroStruct: Enable and Learn How to Integrate Flexibility in Design; Contributions to the Ralf Heinrich Conference proceedings 2018 Springe

[复制链接]
楼主: 漏出
发表于 2025-3-28 18:07:23 | 显示全部楼层
发表于 2025-3-28 21:37:43 | 显示全部楼层
Numerical Computations of Isolated and Installed Engine Jet Flowsuse of the DLR TAU-Code to investigate the complex aerodynamics of jet-flap interactions was devised which also ensures the usability of the RANS (Reynolds Averaged Navier–Stokes) results in a subsequent aeroacoustic analysis.
发表于 2025-3-28 23:23:07 | 显示全部楼层
Further Development of CAA Simulation for Isolated and Installed Nozzle Configurationsnsideration of both noise generation mechanisms simultaneously. Thus, a vorticity based ‘Eddy Relaxation’ source model has been recently proposed as further development of this methodology, which is expected to capture the installation effect.
发表于 2025-3-29 04:12:04 | 显示全部楼层
发表于 2025-3-29 11:11:40 | 显示全部楼层
发表于 2025-3-29 15:03:07 | 显示全部楼层
发表于 2025-3-29 18:03:40 | 显示全部楼层
发表于 2025-3-29 20:53:56 | 显示全部楼层
发表于 2025-3-30 00:49:14 | 显示全部楼层
Ausgangssituation im Anlagenbau,use of the DLR TAU-Code to investigate the complex aerodynamics of jet-flap interactions was devised which also ensures the usability of the RANS (Reynolds Averaged Navier–Stokes) results in a subsequent aeroacoustic analysis.
发表于 2025-3-30 06:55:09 | 显示全部楼层
 关于派博传思  派博传思旗下网站  友情链接
派博传思介绍 公司地理位置 论文服务流程 影响因子官网 SITEMAP 大讲堂 北京大学 Oxford Uni. Harvard Uni.
发展历史沿革 期刊点评 投稿经验总结 SCIENCEGARD IMPACTFACTOR 派博系数 清华大学 Yale Uni. Stanford Uni.
|Archiver|手机版|小黑屋| 派博传思国际 ( 京公网安备110108008328) GMT+8, 2025-5-6 14:45
Copyright © 2001-2015 派博传思   京公网安备110108008328 版权所有 All rights reserved
快速回复 返回顶部 返回列表