An efficient numerical algorithm in the classical 3d theory of thin lifting surface in a flow of non-viscous incompressible fluid-Reference-Cited by-同舟云学术

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An efficient numerical algorithm in the classical 3d theory of thin lifting surface in a flow of non-viscous incompressible fluid

Published:2018-04 Issue: Volume:89 Page:18-22
ISSN:0093-6413
Container-title:Mechanics Research Communications
language:en
Short-container-title:Mechanics Research Communications

Author:

Sumbatyan M.A.^ORCID,Bondarchuk A.A.,Mescheryakov K.I.

Publisher

Elsevier BV

Subject

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

Reference14 articles.

1. Aeroelasticity;Bisplinghoff,1955

2. Prandtl, L. Tragflügeltheorie. konigliche gesellschaft der wissenschaften zu göttingen, 1918.

3. Effect of finite span on the airload distributions for oscillating wings;Reissner,1947

4. Theoretical and experimental pressure distributions on low apsect-ratio wings oscillating in an incompressible flow;Laidlaw,1954

5. Note on the lifting-surface problem for a circular wing in incompressible flow;Boersma;Quart. J. Mech. Appl. Math.,1989

Cited by 1 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. On the theory of thin lifting surface with winglets;Mechanics Research Communications;2020-10

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