Prediction of a Supersonic Wing Flutter Boundary Using a High Fidelity Detached Eddy Simulation

Book chapter

Hongsik Im, Xiangying Chen and Gecheng Zha

50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

2012

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Title: Prediction of a Supersonic Wing Flutter Boundary Using a High Fidelity Detached Eddy Simulation
Creators: Hongsik Im
Xiangying Chen
Gecheng Zha
Publication Details: 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Academic Unit: CoE - Mechanical & Aerospace Engineering; College of Engineering
Language: English
Resource Type: Book chapter
Record Identifier: 991031620151702976