Control of Separation of Flow

Author:

CHANG PAUL K.

Publisher

Elsevier

Reference88 articles.

1. Approximate Methods for Calculating Three-dimensional Boundary Layer Flow on Wings;LINDFIELD,1961

2. A Non-linear Wing Theory and its Application to Rectangular Wings of Small Aspect Ratio;BOLLAY;Z. angew. Math. Mech.,1939

3. Nichtlineare Tragflügel mit kleinem Seitenverhältnis;GERSTEN;Ing.-Archiv,1961

4. Aerodynamics of a Rectangular Plate with Vortex Separation in Supersonic Flow;CHENG;J. Aeronaut. Sci.,1955

Cited by 54 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

1. Impact of Energy Input on the Aerodynamic Characteristics and Heat Flux Occurring in the 3D Supersonic Flow Past a Model Aircraft;Mathematical Models and Computer Simulations;2023-07-25

2. Features of the Flow Structure in the Boundary Layer on the Flying Wing Model;SIBERIAN JOURNAL OF PHYSICS;2023-05-10

3. Numerical Schemes Comparison in Solving the Problem of Laminar Flow in the Suddenly Expanding Channel;Herald of the Bauman Moscow State Technical University. Series Natural Sciences;2023-02

4. The сlarification of fine media by filtration;CONSTRUCTION: THE FORMATION OF LIVING ENVIRONMENT: FORM-2022;2023

5. Hysteresis properties of supersonic flow past an annular cavity at angles of attack;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

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