In order to confirm qualitatively that the experimentally observed, unusual flutter phenomenon for a high-aspect-ratio (non-tailored) forward swept wing model is indeed shock-stall flutter, the aeroelastic response calculation of a two-dimensional airfoil whose vibration characteristics are similar
Numerical simulations of the steady Navier–Stokes equations using adaptive meshing schemes
✍ Scribed by Lili Ju; Hyung-Chun Lee; Li Tian
- Publisher
- John Wiley and Sons
- Year
- 2008
- Tongue
- English
- Weight
- 421 KB
- Volume
- 56
- Category
- Article
- ISSN
- 0271-2091
- DOI
- 10.1002/fld.1549
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