Control of blade flutter by smart-casing treatment

Journal of Propulsion and Power

Volumn 17, Issue 2, 2001, Pages 248-255

  Sun, X ^a   Jing, X ^a   Zhao, H ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC IMPEDANCE; COMPRESSORS; FOURIER TRANSFORMS; MATHEMATICAL MODELS; ORIFICES; TURBOMACHINE BLADES;

MACH NUMBER; SMART CASING TREATMENT;

FLUTTER (AERODYNAMICS);

EID: 0035279747     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5770     Document Type: Article

References (13)

1. Recent developments in flutter suppression techniques for turbomachinery rotors
2. Possibility of cascade flutter suppression by use of nonrigid duct wall
3. Some three-dimensional effects on unsteady aerodynamic forces on oscillating cascades
4. Effects of wall admittance changes on aeroelastic stability of turbomachinery
5. Active control of airfoil flutter
6. On the theory of unsteady high reynolds number flow through a circular aperture
7. Sound absorption caused by vorticity shedding, demonstrated with a jet flow
8. The absorption of sound by perforated linings
9. Experimental investigations of perforated liners with bias flow
10. Active control of wall acoustic impedance
11. Sound attenuation in acoustically lined circular ducts in the presence of uniform flow and shear flow