Aerodynamics of pointed forebodies at high angles of attack
Author:
Affiliation:
1. The University of British Columbia, Vancouver Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44983
Reference27 articles.
1. Lament, P J and Hunt, B L , Pressure and Force Distributions on a Sharp Nosed Circular Cylinder at Large Angles of Inclination to a Uniform Subsonic Stream ' Journal of Fluid Mechanics Vol 76 Pt. 3 1976pp519559
2. 4Ragsdale W C andHoranoff E V Investigation of Side Force Due to Ablation AIAA Journal Vol 16 Sept 1978 pp 1010 1011
3. Ericsson, L E Flow Pulsations on Concave Conic Forebodies Journal of Spacecraft and Rockets Vol 15 Sept Oct 1978pp287292
Cited by 11 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. Side force control on slender body by self-excited oscillation flag;Theoretical and Applied Mechanics Letters;2016-09
2. Helical-Groove and Circular-Trip Effects on Side Force;Journal of Aircraft;2000-09
3. Cobra maneuver unsteady aerodynamic considerations;Journal of Aircraft;1995-01
4. Three-dimensional boundary layer and vortex wake over a cone at high angle of attack: study of asymmetries;Experiments in Fluids;1993-02
5. What makes the Cobra maneuver possible?;31st Aerospace Sciences Meeting;1993-01-11
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