| Authors | Seyyed majid Malek Jafarian |
| Journal | Acta Mechanica Sinica |
| Page number | 1-17 |
| Serial number | 42 |
| Volume number | 324839 |
| IF | 0.749 |
| Paper Type | Full Paper |
| Published At | 2026 |
| Journal Grade | ISI |
| Journal Type | Typographic |
| Journal Country | Belgium |
| Journal Index | JCR،Scopus |
| Keywords | Adaptive time spectral method, Blanked cells, Dynamic hole cutting, Overset grid, Pitching airfoil |
|---|
Abstract
The time spectral approach, a spectral method based on the Fourier series with an appropriate convergence speed, can be
utilized for a time-varying problem like the flow around a pitching airfoil. This approach has the drawback of having a
constant number of time intervals over the entire computational domain, which unnecessarily uses up more computer memory
and central processing unit (CPU) time. By distributing time intervals in the computational domain optimally (proportional to
the flow gradient), the adaptive time spectral approach can overcome the shortcoming of the time spectral method. In the
current study, the adaptive time spectral method is added to an inviscid fluid flow solver. Also, in the airfoil with pitching
motion, a grid known as an overset grid has been used, including two grids with an overlapping region. The results for the
three cases (Cases 1, 2, and 5) of the NACA0012 pitching airfoil with different angles of attack studied by AGARD Institute,
with Mach numbers 0.6, 0.6, and 0.755, respectively, showed that while having an acceptable solution accuracy, the amount of
computer memory and CPU time is significantly reduced compared to the standard time spectral method.
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