Abstract
An optimization method for the determination of the dominant flutter modes is presented in this paper. The method is based on the minimization of the quadratic values of subdeterminants derived from the equations of motion. The effectiveness of the method is illustrated by seven numerical examples.
| Original language | English |
|---|---|
| Pages (from-to) | 663-668 |
| Number of pages | 6 |
| Journal | Journal of Aircraft |
| Volume | 18 |
| Issue number | 8 |
| DOIs | |
| State | Published - Aug 1981 |
| Externally published | Yes |