Our heavyweight helicopter equal in the world does not have
In Rostov started production of the most load-lifting rotary-wing car The Russian holding «Helicopt[...]
Results
2.3 Adaptation by an Adjoint Error Estimate
The adjoint error estimate as sensor for adaptation is tested on two configurations. The first configuration is a clean wing/body configuration of the DLR-F6 geometry
[8, 12]. The second configuration is the high-lift wing/body configuration TC 217 with deployed flaps and slats. For both configurations the numerical results are compared to wind tunnel measurements.
