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Khemiri, Oualid and Martel Escobar, Carlos and Corral, Roque (2011). Forced response of Bladed Disks with Damping Mistuning. In: "ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition (GT2011)", June 6–10, 2011, Vancouver, British Columbia, Canada. https://doi.org/10.1115/GT2011-45802.
Title: | Forced response of Bladed Disks with Damping Mistuning |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition (GT2011) |
Event Dates: | June 6–10, 2011 |
Event Location: | Vancouver, British Columbia, Canada |
Title of Book: | Proceedings of ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition (GT2011) |
Date: | 2011 |
Subjects: | |
Faculty: | E.T.S.I. Aeronáuticos (UPM) |
Department: | Fundamentos Matemáticos de la Tecnología Aeronáutica [hasta 2014] |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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The effect of mistuning on the vibration of bladed disks has been extensively studied in the past 30 years. Most of these analysis typically cover the case of small variations of the elastic characteristics (mass and stiffness) of the blades. In this work we study the not so common case of the forced response of a stable rotor with damping mistuning. The Asymptotic Mistuning Model (AMM) is used to analyze this problem. The AMM methodology provides a simplified model that describes the effect of blade to blade damping variation, and gives precise information on the underlying mechanisms involved in the action of damping mistuning.
Item ID: | 12904 |
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DC Identifier: | https://oa.upm.es/12904/ |
OAI Identifier: | oai:oa.upm.es:12904 |
DOI: | 10.1115/GT2011-45802 |
Deposited by: | Memoria Investigacion |
Deposited on: | 26 Feb 2013 09:24 |
Last Modified: | 22 Sep 2014 10:56 |