Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula-Reference-Cited by-同舟云学术

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Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula

Published:2015-06 Issue:6 Volume:53 Page:1492-1502
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Liu Tianshu¹,Wang Shizhao²,Zhang Xing²,He Guowei²

Affiliation:

1. Department of Mechanical and Aerospace Engineering, Western Michigan University, Kalamazoo, Michigan 49008

2. Institute of Mechanics, State Key Laboratory of Nonlinear Mechanics, Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053439

Reference31 articles.

1. MunkM. M. “Elements of the Wing Section Theory and of the Wing Theory,” NASA Rept. 1050, 1979, pp. 127–149.

2. A New Approach to Thin Aerofoil Theory

3. Über die Entstehung des dynamischen Auftriebes von Tragflügeln

4. TheodorsenT. “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA Rept. 496, 1935.

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