Research Article
Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow
Figure 4
The shapes of the first four modes used in the modal method (the contour plot of the height (unit: m); : streamwise, : spanwise, : height).
(a) The 1st mode |
(b) The 2nd mode |
(c) The 3rd mode |
(d) The 4th mode |