Advanced Structural Analysis Based on Reduced-Order Modeling for Gas Turbine Blade
Author:
Affiliation:
1. Republic of Korea Air Force, Daegu 41052, Republic of Korea
2. Seoul National University, Seoul 08826, Republic of Korea
3. Sejong University, Seoul 05006, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057063
Reference7 articles.
1. Blade Forced Response Prediction for Industrial Gas Turbines
2. AN INTEGRATED NONLINEAR APPROACH FOR TURBOMACHINERY FORCED RESPONSE PREDICTION. PART II: CASE STUDIES
3. Geometrically nonlinear dynamic formulation for three-dimensional co-rotational solid elements
4. Free vibration behavior of spinning shear-deformable plates composedof composite materials
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