Applied Mathematics and Mechanics (English Edition) ›› 2026, Vol. 47 ›› Issue (5): 1177-1204.doi: https://doi.org/10.1007/s10483-026-3381-7
Qihang MA1, Feng FENG2, Bofu WANG1,†(
), Quan ZHOU1
Received:2026-01-17
Revised:2026-03-16
Published:2026-05-06
Contact:
Bofu WANG, E-mail: bofuwang@shu.edu.cnSupported by:2010 MSC Number:
Qihang MA, Feng FENG, Bofu WANG, Quan ZHOU. High-order finite-volume central targeted essentially non-oscillatory schemes for shock-driven flows on unstructured meshes. Applied Mathematics and Mechanics (English Edition), 2026, 47(5): 1177-1204.
Fig. 1
WENO/CWENO stencils on 2D triangular grids: (a) 5th-order central stencil for WENO, (b) 5th-order directional stencils for WENO, and (c) 3rd-order directional stencils for CWENO (the cell under consideration is displayed in red, while the central stencil elements are displayed in gray, and each directional stencil is indicated by a distinct color, where the actual number of cells in the stencil equals twice the polynomial degrees of freedom, as depicted in Eq. (5)) (color online)"
Table 1
Errors and accuracy with 2D Euler equations for CTENO and CTENOZ schemes (h is the number of edges, Ne is the total number of elements, and both L∞ error and L2 error are calculated based on h and Ne, in all figures and tables throughout this paper, CTENO3 denotes the 3rd-order CTENO scheme. Likewise, CTENOZ3 and CTENOZ4 refer to the 3rd-order and 4th-order CTENOZ schemes, respectively, and other notations follow the same rule)"
| h | Ne | L∞ error | L∞ order | L2 error | L2 order | |
|---|---|---|---|---|---|---|
| CTENO3 | 1/10 | 100 | ||||
| CTENOZ3 | 1/20 | 400 | 2.42 | 2.43 | ||
| 1/40 | 1 600 | 2.90 | 2.90 | |||
| 1/80 | 6 400 | 2.98 | 2.98 | |||
| 1/160 | 25 600 | 3.00 | 3.00 | |||
| CTENO4 | 1/10 | 100 | ||||
| CTENOZ4 | 1/20 | 400 | 3.64 | 3.65 | ||
| 1/40 | 1 600 | 3.94 | 3.92 | |||
| 1/80 | 6 400 | 3.99 | 3.97 | |||
| 1/160 | 25 600 | 4.00 | 3.99 | |||
| CTENO5 | 1/10 | 100 | ||||
| CTENOZ5 | 1/20 | 400 | 4.73 | 4.72 | ||
| 1/40 | 1 600 | 4.94 | 4.95 | |||
| 1/80 | 6 400 | 4.99 | 4.99 | |||
| 1/160 | 25 600 | 4.99 | 4.99 | |||
| CTENO6 | 1/10 | 100 | ||||
| CTENOZ6 | 1/20 | 400 | 5.73 | 5.73 | ||
| 1/40 | 1 600 | 6.00 | 5.97 | |||
| 1/80 | 6 400 | 6.01 | 6.01 | |||
| 1/160 | 25 600 | 6.00 | 6.00 | |||
| CTENO7 | 1/10 | 100 | ||||
| CTENOZ7 | 1/20 | 400 | 7.11 | 7.09 | ||
| 1/40 | 1 600 | 6.92 | 6.93 | |||
| 1/80 | 6 400 | 6.84 | 6.84 | |||
| 1/160 | 25 600 | 6.81 | 6.85 |
Fig. 9
Interaction of a shock wave with a cylinder in 2D: results from CTENOZ5 at (a) t=20 μs, (b) t=38 μs, and (c) t=76 μs with regular reflection to Mach reflection shock waves. Results from CTENOZ5 at (d) t=20 μs, (e) t=67 μs, and (f) t=106 μs with Mach reflection shock waves (the figures show density gradient magnitude contours ranging from 0 to 5 000) (color online)"
Fig. 12
3D explosion problem: (a) unstructured tetrahedral elements with cross-sectional density distribution of simulation results, ranging from 0.15 to 1.0 with 18 levels; (b) unstructured hybrid elements with cross-sectional density distribution of simulation results, ranging from 0.15 to 1.0 with 18 levels; (c) density profile compared with exact results; (d) pressure profile compared with exact results (color online)"
Fig. 13
3D explosion problem: (a) numerically generated x-t diagram with numerical results compared with Brode’s results under blast sphere gas flow; (b) cross-sectional density distribution at t=0.19 ms ranging from 2 to 24; (c) cross-sectional density distribution at t=0.3 ms ranging from 2 to 24; (d) cross-sectional pressure profile at t=0.3 ms ranging from 2×105 Pa to 2×106 Pa (color online)"
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