Effect of Acoustic Control on the Flutter Boundaries of Supersonic Cascade-Reference-Cited by-同舟云学术

Effect of Acoustic Control on the Flutter Boundaries of Supersonic Cascade

Published:1998 Issue: Volume: Page:165-179
ISSN:
Container-title:Unsteady Aerodynamics and Aeroelasticity of Turbomachines
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Author:

Nagai K.,Namba M.

Publisher

Springer Netherlands

Link

http://link.springer.com/content/pdf/10.1007/978-94-011-5040-8_11

Reference8 articles.

1. Ffowcs Williams, J.E. (1984) Review Lecture: Anti-Sound, Proceedings of the Royal Society of London, A395, pp.63–88.

2. Ffowcs Williams, J.E. (1989) Active Control of Engine Instabilities, Proceedings of 9th International Symposium on Air Breathing Engines, Vol.1, pp.45–48.

3. 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.

4. 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.

5. 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.

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