Table 5.
Comparison of main design parameters or sub-models of aircraft before and after CDM.
| Mex | Ns | Bd(mm) | Hn(mm) | Wn(mm) | Bu(mm) | |
|---|---|---|---|---|---|---|
| m0 | Mex1 | 1 | Xv = 500 | 330 | 800 | Xu = 300 |
| M* | Mex3 | 2 | Xv = 1150 | 300 | 950 | Xu = 400 |
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