Abstract
In our recent study of strip plate flutter, two flutter types, low-and high-frequency, were revealed. The first arises due to interaction of the oscillation modes and has been investigated in detail in numerous studies using an approximate piston theory. The high-frequency flutter, detected for the first time, is a consequence of the presence of negative aerodynamic damping and cannot be obtained using the piston theory. In the present study, the high-frequency flutter of a rectangular plate is investigated.
Similar content being viewed by others
References
V. V. Vedeneev, “Flutter of a wide strip plate in a supersonic gas flow,” Fluid Dynamics, 40, No. 5, 805–817 (2005).
V. V. Vedeneev, “High-frequency plate flutter,” Fluid Dynamics, 41, No. 2, 313–321 (2006).
A. G. Kulikovskii, “On the stability of homogeneous states,” Prikl. Mat. Mekh., 30, No. 1, 148–153 (1966).
E. M. Lifshits and L. P. Pitaevskii, Theoretical Physics. V. 10. Physical Kinetics [in Russian], Nauka, Moscow (1979).
A. G. Kulikovskii, “On the global instability of homogeneous flows in more than one-dimensional domains,” Prikl. Mat. Mekh., 70, No. 2, 257–263 (2006).
V. L. Biderman, Theory of Mechanical Oscillations [in Russian], Vysshaya Shkola, Moscow (1980).
Additional information
__________
Translated from Izvestiya Rossiiskoi Academii Nauk, Mekhanika Zhidkosti i Gaza, No. 4, 2006, pp. 173–181.
Original Russian Text Copyright © 2006 by Vedeneev.
Rights and permissions
About this article
Cite this article
Vedeneev, V.V. High-frequency flutter of a rectangular plate. Fluid Dyn 41, 641–648 (2006). https://doi.org/10.1007/s10697-006-0083-2
Received:
Issue Date:
DOI: https://doi.org/10.1007/s10697-006-0083-2