TY - GEN
T1 - Computation of the optimal normal load of a friction damper under different types of excitation
AU - Cha, D.
AU - Sinha, A.
N1 - Publisher Copyright:
Copyright © 1999 by ASME.
PY - 1999
Y1 - 1999
N2 - In this paper, forced responses of a frictionally damped turbine blade are investigated for three different types of excitation: white noise excitation, narrow band random excitation and deterministic sinusoidal excitation. To determine the steady state nonlinear response, the harmonic balance method is used for sinusoidal excitation, and the equivalent linearization method is used for white noise and narrow band random excitations. Using a new set of nondimensionalized variables, the optimal value of normal load of a friction damper is found to be almost independent of the nature of excitation. The effectiveness of the damper in reducing the vibration level is also examined for the aforementioned three different types of excitation.
AB - In this paper, forced responses of a frictionally damped turbine blade are investigated for three different types of excitation: white noise excitation, narrow band random excitation and deterministic sinusoidal excitation. To determine the steady state nonlinear response, the harmonic balance method is used for sinusoidal excitation, and the equivalent linearization method is used for white noise and narrow band random excitations. Using a new set of nondimensionalized variables, the optimal value of normal load of a friction damper is found to be almost independent of the nature of excitation. The effectiveness of the damper in reducing the vibration level is also examined for the aforementioned three different types of excitation.
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U2 - 10.1115/99-GT-413
DO - 10.1115/99-GT-413
M3 - Conference contribution
AN - SCOPUS:84928529841
T3 - Proceedings of the ASME Turbo Expo
BT - Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition, GT 1999
Y2 - 7 June 1999 through 10 June 1999
ER -