Projects per year
Abstract
This work proposes a extends a novel approach to compute tran
sonic Limit Cycle Oscillations using high fidelity analysis. CFD based Harmonic
Balance methods have proven to be efficient tools to predict periodic phenomena. This paper’s contribution is to present a methodology to determine the unknown frequency of oscillations using an implicit for-
mulation of the HB method to accurately capture Limit Cycle Oscillations (LCOs); this is achieved by defining a frequency updating procedure based
on a coupled CFD/CSD Harmonic Balance formulation to find the LCO condition. A pitch/plunge aerofoil and respective linear structural models is used to exercise the new method. Results show consistent agreement between the proposed and time-marching methods for both LCO amplitude and frequency.
Original language | English |
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Publication status | Published - 08 Oct 2014 |
Event | Royal Aeronautical Society Aircraft 4th Structural Design Conference - Belfast, United Kingdom Duration: 07 Oct 2014 → 09 Oct 2014 |
Conference
Conference | Royal Aeronautical Society Aircraft 4th Structural Design Conference |
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Country/Territory | United Kingdom |
City | Belfast |
Period | 07/10/2014 → 09/10/2014 |
Keywords
- CFD
- Harmonic Balance
- Aeroelasticity
- LCO
ASJC Scopus subject areas
- Aerospace Engineering
Fingerprint
Dive into the research topics of 'Prediction of Limit Cycle Oscillations Using an Implicit Aeroelastic-Harmonic Balance Method'. Together they form a unique fingerprint.Projects
- 1 Finished
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R1191AER: ENACT - Efficient non-linear Aeroelasticity Computations under Uncertainty
Marques, S. (PI)
01/08/2012 → 31/12/2014
Project: Research
Research output
- 1 Paper
-
Prediction of Transonic LCOs using an Aeroelastic Harmonic Balance Method
Yao, W. & Marques, S., 18 Jun 2014.Research output: Contribution to conference › Paper › peer-review
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