Recent Advancements in Turbomachinery Aeroelastic Design Analysis
Author:
Affiliation:
1. Duke University
2. CD-adapco
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-14
Reference33 articles.
1. Numerical Computation of Nonstationary Aerodynamics of Flat Plate Cascades in Compressible Flow
2. Calculation of unsteady flows in turbomachinery using the linearizedEuler equations
3. 2D Linearized Harmonic Euler Flow Analysis for Flutter and Forced Response
4. Time Linearized Euler Calculations for Unsteady Quasi-3D Cascade Flows
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1. A parametric study of Limit Cycle Oscillation of a bladed disk caused by flutter and friction at the blade root joints;Journal of Fluids and Structures;2018-01
2. Reduced order unsteady aerodynamic modeling for stability and control analysis using computational fluid dynamics;Progress in Aerospace Sciences;2014-11
3. Forced Response Analysis of Compressor Blades under Unsteady Inlet Distortion;31st AIAA Applied Aerodynamics Conference;2013-06-22
4. Analysis of Flutter-Induced Limit Cycle Oscillations in Gas-Turbine Structures With Friction, Gap, and Other Nonlinear Contact Interfaces;Journal of Turbomachinery;2012-09-04
5. Volterra kernel identification of MIMO aeroelastic system through multiresolution and multiwavelets;Computational Mechanics;2011-10-29
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