Probabilistic Study of Integrally Bladed Rotor Blends using Geometric Mistuning Models
Author:
Affiliation:
1. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0860
Reference36 articles.
1. Discussion: “Eccentricity Effects on the Rotordynamic Coefficients of Plain Annular Seals: Theory Versus Experiment” (Marquette, O. R., Childs, D. W., and San Andres, L., 1997, ASME J. Tribol., 119, pp. 443–447)
2. A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes
3. A Reduced Order Approach for the Vibration of Mistuned Bladed Disk Assemblies
4. A Fundamental Model of Mistuning for a Single Family of Modes
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