Plasma-Based Control of Excrescence-Generated Transition on a Swept Wing

Author:

Rizzetta Donald P.1,Visbal Miguel R.1

Affiliation:

1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference50 articles.

1. HoodM. J. “The Effects of Surface Waviness and of Rib Stitching on Wing Drag,” NACA Langley Aeronautical Lab. TN 724, Langley Field, VA, Aug. 1939.

2. FageA. “The Smallest Size of a Spanwise Surface Corrugation Which Affects Boundary-Layer Transition on an Aerofoil,” Aeronautical Research Council, Reports and Memoranda 2120, Jan. 1943.

3. GregoryN.WalkerW. S.JohnsonD. “Part I: The Effect on Transition of Isolated Surface Excrescences in the Boundary Layer; Part II: Brief Flight Tests on a VampireI Aircraft to Determine the Effect of Isolated Surface Pimples on Transition,” Aeronautical Research Council, Reports and Memoranda 2779, Oct. 1951.

4. SmithA. M. O.ClutterD. W. “The Smallest Height of Roughness Capable of Affecting Boundary-Layer Transition in Low-Speed Flow,” Douglas Aircraft Co., Engineering Rept. ES26803, 1954.

5. BraslowA. L. “The Effect of Distributed Surface Roughness on Boundary-Layer Transition,” NATO, AGARD Rept. 254, Jan. 1960.

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

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