Multidisciplinary Design Optimization of Transonic Wings with Boundary-Layer Suction
Author:
Affiliation:
1. University of Braunschweig—Institute of Technology, 38108 Braunschweig, Germany
2. University of California, Davis, Davis, California 95616
3. University of Southampton, Southampton, England SO16 7QF, United Kingdom
Abstract
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C037362
Reference64 articles.
1. BraslowA. L. “Europe’s Vision for Aviation: Maintaining Global Leadership and Serving Society’s Needs,” Flightpath 2050, European Commission and Directorate-General for Mobility and Transport and Directorate-General for Research and Innovation, Luxembourg, 2011. 10.2777/50266
2. BraslowA. L. “A History of Suction-Type Laminar Flow Control with Emphasis on Flight Research,” NASA Monographs in Aerospace History No. 13, 1999.
3. Experimental and theoretical study of swept-wing boundary-layer instabilities. Three-dimensional Tollmien-Schlichting instability
4. The role of stationary cross‐flow vortices in boundary‐layer transition on swept wings
5. Shock boundary-layer interaction on transonic airfoils for laminar and turbulent flow
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3