Prediction of wing flutter boundary using high fidelity delayed detached eddy simulation

Jia Ye Gan, Hong Sik Im, Xiang Ying Chen, GeCheng Zha, Crystal L. Pasiliao

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper conducts Delayed Detached Eddy Simulation(DDES) of a 3D wing flutter with free stream Mach number varied from subsonic to supersonic using a fully coupled fluid/structure interaction (FSI). Unsteady 3D compressible Navier-Stokes equations are solved with a system of 5 decoupled structure modal equations in a fully coupled manner. The low diffusion E-CUSP scheme with a 5th order WENO reconstruction for the inviscid flux and a set of 4th order central differencing for the viscous terms are used to accurately capture the shock wave/turbulent boundary layer interaction of the vibrating wing. The predicted flutter boundaries at different free stream Mach numbers achieve very good agreement with experiment. It appears that the transonic dip phenomenon is due to the anticlimax contribution of the second mode, which is caused by the complicated shock oscillation on the wing.

Original languageEnglish (US)
Title of host publication56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624103421
StatePublished - 2015
Event56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 - Kissimmee, United States
Duration: Jan 5 2015Jan 9 2015

Other

Other56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015
CountryUnited States
CityKissimmee
Period1/5/151/9/15

Fingerprint

Flutter (aerodynamics)
Mach number
Fluid structure interaction
Shock waves
Navier Stokes equations
Boundary layers
Fluxes
Experiments

ASJC Scopus subject areas

  • Civil and Structural Engineering
  • Architecture
  • Mechanics of Materials
  • Building and Construction

Cite this

Gan, J. Y., Im, H. S., Chen, X. Y., Zha, G., & Pasiliao, C. L. (2015). Prediction of wing flutter boundary using high fidelity delayed detached eddy simulation. In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference American Institute of Aeronautics and Astronautics Inc..

Prediction of wing flutter boundary using high fidelity delayed detached eddy simulation. / Gan, Jia Ye; Im, Hong Sik; Chen, Xiang Ying; Zha, GeCheng; Pasiliao, Crystal L.

56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc., 2015.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Gan, JY, Im, HS, Chen, XY, Zha, G & Pasiliao, CL 2015, Prediction of wing flutter boundary using high fidelity delayed detached eddy simulation. in 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc., 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015, Kissimmee, United States, 1/5/15.
Gan JY, Im HS, Chen XY, Zha G, Pasiliao CL. Prediction of wing flutter boundary using high fidelity delayed detached eddy simulation. In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc. 2015
Gan, Jia Ye ; Im, Hong Sik ; Chen, Xiang Ying ; Zha, GeCheng ; Pasiliao, Crystal L. / Prediction of wing flutter boundary using high fidelity delayed detached eddy simulation. 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics Inc., 2015.
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