Thesis etd-11062015-134820 |
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Thesis type
Tesi di laurea magistrale
URN
etd-11062015-134820
Thesis title
3D study of the stall behavior of a high-wing aircraft equipped with Coanda-flap and droop-nose devices
Department
INGEGNERIA CIVILE E INDUSTRIALE
Course of study
INGEGNERIA AEROSPAZIALE
Supervisors
.
relatore Prof. Lombardi, Giovanni
correlatore Prof. Radespiel, Rolf
correlatore Ing. Burnazzi, Marco
correlatore Ing. Brühl, Markus
correlatore Prof. Radespiel, Rolf
correlatore Ing. Burnazzi, Marco
correlatore Ing. Brühl, Markus
Keywords
- Active High-Lift Devices
- CFD
- Coanda-flap
- Droop nose
- High-wing aircraft
- RANS
- SFB 880
Graduation session start date
01/12/2015
Availability
Full
Abstract (Inglese)
Abstract (Italiano)
The present work focuses on the evaluation of the stall performances of the reference aircraft concept of the Collaborative Research Center SFB (Sonderforschungsbereich) 880, by means of CFD RANS simulations.
Two new configurations of the SFB 880 aircraft, obtained from a previous geometry model, have been analyzed and discussed. The purpose was to investigate the influence of the leading edge connection with the fuselage on the cross flow that takes place between the fuselage and the suction side of the wing and affects the aircraft stall behavior.
Two new configurations of the SFB 880 aircraft, obtained from a previous geometry model, have been analyzed and discussed. The purpose was to investigate the influence of the leading edge connection with the fuselage on the cross flow that takes place between the fuselage and the suction side of the wing and affects the aircraft stall behavior.
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