Flutter Limits and Behaviors of a Flexible Thin Sheet in High-Speed Flow— I: Analytical Method for Prediction of the Sheet Behavior

Author:

Yamaguchi Nobuyuki1,Yokota Kazuhiko,Tsujimoto Yoshinobu2

Affiliation:

1. Department of Mechanical Engineering, Meisei University, Hino City, Tokyo 191-8506, Japan

2. Department of Mechanical Engineering, Faculty of Engineering Science, Osaka University, Toyonaka City 560-8531, Japan

Abstract

An analytical method is proposed for the prediction of fluttering of a flexible thin sheet or web swept by fluid flow. It assumes self-excited aeroelastic oscillation of the sheet with infinitesimally small amplitude. The flow and the sheet motion are expressed by distributed vortices over the sheet and the wake, and by bending motions of a number of short segments constituting the sheet. The obtained system of equations determines the flutter limits, the oscillation modes and frequencies. The method treats particularly well the situation of very low mass ratios where the modes are far from those in vacuum and progressive waves are predominant. [S0098-2202(00)01101-9]

Publisher

ASME International

Subject

Mechanical Engineering

Reference24 articles.

1. Theodorsen, T., 1935, “General Theory of Aerodynamic Instability and the Mechanism of Flutter,” NACA Report No. 496.

2. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., 1955, Aeroelasticity, Addison-Wesley, Cambridge, MA.

3. Fung, Y. C., 1995, An Introduction to the Theory of Aeroelasticity, Wiley, New York.

4. Bisplinghoff, R. L., and Ashley, H., 1962, Principles of Aeroelasticity, Wiley, New York.

5. Dowell, E. H., 1975, Aeroelasticity of Plates and Shells, Noordhoff International Publishing, Leyden, The Netherlands.

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