Research Article
Finite Element Analysis on Acoustic and Mechanical Performance of Flexible Perforated Honeycomb-Corrugation Hybrid Sandwich Panel
Figure 15
The steady-state stress distribution after being subjected to the same shear load. The deformation is enlarged 1 × 107, 1 × 108, and 1 × 108 times from (a) to (c), respectively.
(a) |
(b) |
(c) |