Abstract
This paper presents a strategy using a high fidelity delayed-detached-eddy simulation (DDES) to simulate 3-D fluid-structural interaction for predicting AGARD Wing 445.6 flutter boundary in a transonic flow. A dual-time step implicit unfactored Gauss-Seidel iteration with Roe scheme are employed for the flow solver. The special numerical techniques used herein include: a 5th order WENO scheme for the inviscid fluxes, and a fully conservative 4th order central differencing scheme for the viscous terms. A modal approach is used for the structural response. The flow and structural solvers are fully coupled vis successive iterations within each physical time step. The method is implemented as a massive parallel solver in a MPI environment. The computed flutter boundary of AGARD Wing 445.6 in a transonic flow agrees well with the experiment and the prediction made by other method.
| Original language | English |
|---|---|
| Title of host publication | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
| State | Published - Dec 14 2010 |
| Event | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition - Orlando, FL, United States Duration: Jan 4 2010 → Jan 7 2010 |
Other
| Other | 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition |
|---|---|
| Country | United States |
| City | Orlando, FL |
| Period | 1/4/10 → 1/7/10 |
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Keywords
- Delayed-detached-eddy simulation
- Fluid-structural interaction
- Transonic wing flutter
ASJC Scopus subject areas
- Aerospace Engineering
Cite this
Delayed detached eddy simulation of 3-D wing flutter with fully coupled fluid-structural interaction. / Chen, Xiangying; Wang, Baoyuan; Zha, GeCheng.
48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. 2010-0053.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Delayed detached eddy simulation of 3-D wing flutter with fully coupled fluid-structural interaction
AU - Chen, Xiangying
AU - Wang, Baoyuan
AU - Zha, GeCheng
PY - 2010/12/14
Y1 - 2010/12/14
N2 - This paper presents a strategy using a high fidelity delayed-detached-eddy simulation (DDES) to simulate 3-D fluid-structural interaction for predicting AGARD Wing 445.6 flutter boundary in a transonic flow. A dual-time step implicit unfactored Gauss-Seidel iteration with Roe scheme are employed for the flow solver. The special numerical techniques used herein include: a 5th order WENO scheme for the inviscid fluxes, and a fully conservative 4th order central differencing scheme for the viscous terms. A modal approach is used for the structural response. The flow and structural solvers are fully coupled vis successive iterations within each physical time step. The method is implemented as a massive parallel solver in a MPI environment. The computed flutter boundary of AGARD Wing 445.6 in a transonic flow agrees well with the experiment and the prediction made by other method.
AB - This paper presents a strategy using a high fidelity delayed-detached-eddy simulation (DDES) to simulate 3-D fluid-structural interaction for predicting AGARD Wing 445.6 flutter boundary in a transonic flow. A dual-time step implicit unfactored Gauss-Seidel iteration with Roe scheme are employed for the flow solver. The special numerical techniques used herein include: a 5th order WENO scheme for the inviscid fluxes, and a fully conservative 4th order central differencing scheme for the viscous terms. A modal approach is used for the structural response. The flow and structural solvers are fully coupled vis successive iterations within each physical time step. The method is implemented as a massive parallel solver in a MPI environment. The computed flutter boundary of AGARD Wing 445.6 in a transonic flow agrees well with the experiment and the prediction made by other method.
KW - Delayed-detached-eddy simulation
KW - Fluid-structural interaction
KW - Transonic wing flutter
UR - http://www.scopus.com/inward/record.url?scp=78649941320&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=78649941320&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:78649941320
SN - 9781600867392
BT - 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
ER -