Abstract
The assimilation of discrete data points with model predictions can be used to achieve a reduction in the uncertainty of the model input parameters which generate accurate predictions. The problem investigated here involves the prediction of limit-cycle oscillations using a High-Dimensional Harmonic Balance method (HDHB). The efficiency of the HDHB method is exploited to enable calibration of structural input parameters using a Bayesian inference technique. Markov-chain Monte Carlo is employed to sample the posterior distributions. Parameter estimation is carried out on a pitch/plunge aerofoil and two Goland wing configurations. In all cases significant refinement was achieved in the distribution of possible structural parameters allowing better predictions of their true deterministic values. Additionally, a comparison of two approaches to extract the true values from the posterior distributions is presented.
| Original language | English |
|---|---|
| Number of pages | 30 |
| Journal | The Aeronautical Journal |
| Early online date | 23 May 2017 |
| DOIs | |
| Publication status | Early online date - 23 May 2017 |
Keywords
- Limit Cycle Oscillation
- aeroelasticity
- uncertainty
- Bayesian Updating
ASJC Scopus subject areas
- Aerospace Engineering
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