Abstract
The statistics of the forced response of a structurally and aerodynamically coupled bladed disk assembly have been computed efficiently by the analytical technique. The validity of the analytical technique has been corroborated by comparison with the results from numerical simulations. Lastly, the effects of the following parameters on the statistics of the maximum amplitude have been studied: aerodynamic coupling, fluid density, and stagger angle.
| Original language | English (US) |
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| Pages (from-to) | GT205 6p |
| Journal | American Society of Mechanical Engineers (Paper) |
| State | Published - Jan 1 1990 |
| Event | International Gas Turbine and Aeroengine Congress and Exposition - Brussels, Belg Duration: Jun 11 1990 → Jun 14 1990 |
All Science Journal Classification (ASJC) codes
- Mechanical Engineering