Calculation of the flow past a delta wing in the thin shock layer approximation-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Calculation of the flow past a delta wing in the thin shock layer approximation

Published:1989-01 Issue:5 Volume:29 Page:195-200
ISSN:0041-5553
Container-title:USSR Computational Mathematics and Mathematical Physics
language:en
Short-container-title:USSR Computational Mathematics and Mathematical Physics

Author:

Golubkin V.N.,Negoda V.V.

Publisher

Elsevier BV

Subject

General Engineering

Reference15 articles.

1. The Newton-theoretical lift of a slender delta wing;Messiter;Raketnaya Tekhn. i Kosmonavtika,1963

2. Thickness effect on the force of slender delta wings in hypersonic flow;Hida;AIAA J.,1965

3. Calculated pressure distributions and shock shapes on thick conical wings at high supersonic speeds;Squire;Aeronaut. Quart.,1967

4. Numerical studies on hypersonic delta wings with detached shock waves;Shanbhas;ARC Current Paper, No. 1277,1974

5. Nonlinear Conical Gas Flows;Bulakh,1970

Cited by 2 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. Optimum lifting body shapes in hypersonic flow at high angles of attack;Theoretical and Computational Fluid Dynamics;1995-01

2. Optimum wing shapes in a hypersonic nonequilibrium flow;Journal of Applied Mechanics and Technical Physics;1993

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