Unsteady transonic flow calculations for wing-fuselage configurations
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-862
Reference18 articles.
1. Subsonic Steady and Oscillatory Aerodynamics for Multiple Interfering Wings and Bodies
2. 'woodward, F. A. "Analysis and Design of W i ng-Body Combinations at Subsonic and Supersonic Speeds." Journal o f A i rcraft, Vol .5, No.6, November - December, 1968, pp. 528-524.
3. Bailey, F. R.; and Ballhaus, W. F. "Relaxation Methods for Transonic Flow About W ing-Cyl inder Combinations and Lifting Swept Wings." Lecture Notes i n Physics, Vol.19, Sprin erVerlag, 1972, pp.2-9.
Cited by 6 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. Transonic flow computations using nonlinear potential methods;Progress in Aerospace Sciences;2000-01
2. Computational Methods for Unsteady Transonic Flows;Unsteady Transonic Aerodynamics;1989-01-01
3. Unsteady transonic flow simulation on a full-span-wing-body configuration;AIAA Journal;1988-12
4. Computation of steady and unsteady vortex-dominated flows with shockwaves;AIAA Journal;1988-05
5. Euler calculations for wing-alone configuration;Journal of Aircraft;1988-05
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