Abstract
This article summarizes the results of an investigation to establish the impact of mistuning on the perfomance and design of blade to blade friction dampers of the type used to control the resonant response of turbine blades in gas turbine engines. In addition, it discusses the importance of friction slip force variations on the dynamic response of shrouded fan blades. (A)
Original language | English (US) |
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Journal | [No source information available] |
State | Published - Jan 1 1984 |
All Science Journal Classification (ASJC) codes
- Mechanical Engineering