INFLUENCE OF FRICTION DAMPERS ON TORSIONAL BLADE FLUTTER.
Publication
, Conference
Sinha, A; Griffin, JH; Kielb, RE
Published in: American Society of Mechanical Engineers Paper
January 1, 1985
A discussion is presented on the stabilizing effects of dry friction on torsional blade flutter. A lumped parameter model with single degree of freedom per blade has been used to represent the rotor stage. The well-known cascade theories for incompressible and supersonic flows have been used to determine the allowable increase in fluid velocity relative to the blade. It has been found that the effectiveness of friction dampers in controlling flutter can be substantial.
Duke Scholars
Published In
American Society of Mechanical Engineers Paper
ISSN
0402-1215
Publication Date
January 1, 1985
Citation
APA
Chicago
ICMJE
MLA
NLM
Sinha, A., Griffin, J. H., & Kielb, R. E. (1985). INFLUENCE OF FRICTION DAMPERS ON TORSIONAL BLADE FLUTTER. In American Society of Mechanical Engineers Paper.
Sinha, A., J. H. Griffin, and R. E. Kielb. “INFLUENCE OF FRICTION DAMPERS ON TORSIONAL BLADE FLUTTER.” In American Society of Mechanical Engineers Paper, 1985.
Sinha A, Griffin JH, Kielb RE. INFLUENCE OF FRICTION DAMPERS ON TORSIONAL BLADE FLUTTER. In: American Society of Mechanical Engineers Paper. 1985.
Sinha, A., et al. “INFLUENCE OF FRICTION DAMPERS ON TORSIONAL BLADE FLUTTER.” American Society of Mechanical Engineers Paper, 1985.
Sinha A, Griffin JH, Kielb RE. INFLUENCE OF FRICTION DAMPERS ON TORSIONAL BLADE FLUTTER. American Society of Mechanical Engineers Paper. 1985.
Published In
American Society of Mechanical Engineers Paper
ISSN
0402-1215
Publication Date
January 1, 1985