Adjoint Harmonic Sensitivities for Forced Response Minimization
Author:
Affiliation:
1. Oxford University Computing Laboratory, University of Oxford, Oxford OX1 2QD, UK
2. Aerothermal Methods Group, Rolls-Royce plc., P.O. Box 31, Derby DE24 8BJ, UK
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/128/1/183/5705773/183_1.pdf
Reference33 articles.
1. Review of Unsteady Aerodynamic Methods for Turbomachinery Aeroelastic and Aeroacoustic Applications;Verdon;AIAA J.
2. A Review of Aeroelasticity Methods With Emphasis on Turbomachinery Applications;Marshall;J. Fluids Struct.
3. An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction. Part II: Case Studies;Vahdati;J. Fluids Struct.
4. Giles, M. B. , 1992, “An Approach for Multi-Stage Calculations Incorporating Unsteadiness,” ASME Paper No. 92-GT-282.
5. Deforming Grid Variational Principle for Unsteady Small Disturbance Flows in Cascades;Hall;AIAA J.
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1. Efficient Forced Response Minimization Using a Full-Viscosity Discrete Adjoint Harmonic Balance Method;AIAA Journal;2024-09-03
2. Multi-Objective Aerodynamic and Aeroelastic Coupled Design Optimization Using a Full Viscosity Discrete Adjoint Harmonic Balance Method;Journal of Turbomachinery;2023-07-27
3. Forced Response Sensitivity Analysis Using an Adjoint Harmonic Balance Solver;Journal of Turbomachinery;2019-01-21
4. A discrete adjoint harmonic balance method for turbomachinery shape optimization;Aerospace Science and Technology;2014-12
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