Abstract
The active acoustic control of the supersonic cascade flutter under steady loading is studied. A three-dimensional linear cascade of blades oscillating in a supersonic flow between parallel walls is considered. The effect of steady loading, i.e., angle of attack, camber and thickness on the unsteady aerodynamic force is dealt with on the basis of the double linearization theory. One of the walls is partially made of actuator surface like a loudspeaker which generates sound waves at the same frequency as that of the blade oscillation, so that the unsteady aerodynamic force due to acoustic disturbances generated from the actuator surface cancels the existing unsteady force on the blades due to blade motions themselves. The optimum condition of the actuator surface geometry and motion is investigated and the capability to enlarge the flutter free domain is demonstrated.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Ffowcs Williams, J.E. (1984) Review Lecture: Anti-Sound, Proceedings of the Royal Society of London, A395, pp.63–88.
Ffowcs Williams, J.E. (1989) Active Control of Engine Instabilities, Proceedings of 9th International Symposium on Air Breathing Engines, Vol.1, pp.45–48.
Nagai, K., Toshimitsu, K. and Namba, M. (1995) Active Supression of Cascade Flutter by Means of Sound Waves from Duct Wall Actuator Surface, Unsteady Aerodynamics and Aeroelasticity of Turbomachines, Elsevier Science B.V., pp.565-581.
Nagai, K. and Namba, M. (1995) Acoustic Control of Subsonic Cascade Flutter in Bending Motion, Proceedings of the 12th International Symposium on Air Breathing Engines, Vol.2, pp.992–1000.
Nagai, K. and Namba, M. (1996) Active Control of Cascade Flutter by Means of Sound Waves from Duct Wall Sources, JSME International Journal, Vol.39, No.3, pp.608–614.
Nagai, K. and Namba, M. (1996) Active Control of Supersonic Cascade Flutter by Sound Waves from Actuator Surface, Transactions of JSME, Series B, Vol.62, No.604, pp.4119–4126.
Namba, M. and Toshimitsu, K. (1991) Double Linearization Theory of Three-Dimensional Cascades with Vibrating Blades under Spanwise-Nonuniform Mean Loading, II: Supersonic Flow, Journal of Sound and Vibration, Vol.148, No.1, pp.69–102.
Namba, M. and Yamasaki, N. (1987) Effect of Sound Absorbing Wall Liners on Unsteady Aerodynamic Forces of a Cascade in a Supersonic Flow, Transactions of JSME, Series B, Vol.53, No.492, pp.2281–2288.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1998 Springer Science+Business Media Dordrecht
About this paper
Cite this paper
Nagai, K., Namba, M. (1998). Effect of Acoustic Control on the Flutter Boundaries of Supersonic Cascade. In: Fransson, T.H. (eds) Unsteady Aerodynamics and Aeroelasticity of Turbomachines. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-5040-8_11
Download citation
DOI: https://doi.org/10.1007/978-94-011-5040-8_11
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-6116-2
Online ISBN: 978-94-011-5040-8
eBook Packages: Springer Book Archive