Asymptotic Description of Maximum Mistuning Amplification of Bladed Disk Forced Response
Author:
Affiliation:
1. ETSI Aeronáuticos, Universidad Politécnica de Madrid, 28040 Madrid, Spain
2. Industria de Turbopropulsores S.A., 28830 Madrid, Spain
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.2968868/5489393/022506_1.pdf
Reference22 articles.
1. Forced Response of Bladed Disk Assemblies: A Survey;Slater;Shock Vib. Dig.
2. Modeling and Analysis of Mistuned Bladed Disk Status and Emerging Directions;Castanier;J. Propul. Power
3. Effect of Mistuning on the Vibration of Turbomachine Blades Induced by Wakes;Whitehead;J. Mech. Eng. Sci.
4. A Novel Perturbation-Based Approach for the Accurate Prediction of the Forced Response of Mistuned Bladed Disks;Han
5. Expedient Estimation of the Maximum Amplification Factor in Damped Mistuned Bladed Disks;Han
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