Low-Engine-Order Excitation Mechanisms in Axial-Flow Turbomachinery
Author:
Affiliation:
1. Analytical Methods, Inc., Redmond, Washington 98052
2. Rolls–Royce, plc., Derby, England DE24 8BJ, United Kingdom
3. Imperial College London, London, England SW7 2BX, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6160
Reference20 articles.
1. Model Development and Statistical Investigation of Turbine Blade Mistuning
2. A New Method for Dynamic Analysis of Mistuned Bladed Disks Based on the Exact Relationship Between Tuned and Mistuned Systems
3. An Analysis System for Blade Forced Response
4. Calculation of unsteady wake/rotor interaction
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