Abstract
A simulation approach is used to demonstrate that an airborne, forward-looking lidar can detect trailing wake vortices generated by a leading aircraft. Computational fluid dynamics techniques are used to generated flowfields containing wake vortices. These flowfields are applied to a Doppler lidar simulation model. The simulated geometry has the forward-looking lidar mounted on a following aircraft, whereas the wake vortices are generated by a leading aircraft. In such a configuration, it is not possible to directly detect the strong rotational velocity components of a wake vortex with a Doppler system; detection relies on the presence of induced axial velocity signatures. We demonstrate that axial flows are induced as the vortices evolve, and that these axial flows can be detected with a Doppler lidar system.
| Original language | English |
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| Pages (from-to) | 984-993 |
| Number of pages | 10 |
| Journal | Journal of Aircraft |
| Volume | 37 |
| Issue number | 6 |
| DOIs | |
| Publication status | Published - 2000 |