Subsonic flow past a thin airfoil in a wind tunnel-Reference-Cited by-同舟云学术

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Subsonic flow past a thin airfoil in a wind tunnel

Published:1991-03 Issue:2-3 Volume:18 Page:129-134
ISSN:0093-6413
Container-title:Mechanics Research Communications
language:en
Short-container-title:Mechanics Research Communications

Author:

Dragoş L.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Civil and Structural Engineering

Reference4 articles.

1. Method of fundamental solutions in plane steady linear aerodynamics;Dragoş;Acta Mechanica,1983

2. An introduction to the theory of infinite series;Bromwich,1949

3. Tables of integrals, summs, series and products (in Russian);Gradstein,1979

4. L. Dragoş, A numerical solution of the equation of thin airfoil in ground effects, accepted for publication in AIAA Journ.

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. The Infinite Span Airfoil in Subsonic Flow;Mathematical Methods in Aerodynamics;2003

2. The application of the boundary integral equations method to subsonic flow with circulation past thin airfoils in a wind tunnel;Acta Mechanica;1994-03

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