Numerical simulations of wings in unsteady flows
MetadataShow full item record
The unsteady vortex-lattice method is further used to investigate the effect of trailing vortices from a large leading wing on a trailing aircraft. The aerodynamic response of the trailing aircraft is examined by calculating the lift and drag forces and the pitch and roll moments. Furthermore, the aerodynamic response and the behavior of the wakes of the crossing wings are investigated.
- Doctoral Dissertations