Prediction of a Supersonic Wing Flutter Boundary Using a High Fidelity Detached Eddy Simulation
Prediction of a Supersonic Wing Flutter Boundary Using a High Fidelity Detached Eddy Simulation
- New search for: Im, H.
- New search for: Chen, X.
- New search for: Zha, G.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: Im, H.
- New search for: Chen, X.
- New search for: Zha, G.
- New search for: American Institute of Aeronautics and Astronautics
Document information
Prediction of a Supersonic Wing Flutter Boundary Using a High Fidelity Detached Eddy Simulation
50th, Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 2012 ; Nashville, TN
Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 501-520
2012-01-01
20 pages
Includes bibliographical references and index
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Similar titles
| British Library Conference Proceedings | 2015