Helicopter fuselage model drag reduction by active flow control systems

F De Gregorio - Journal of the American Helicopter Society, 2019 - ingentaconnect.com
A comprehensive experimental investigation of a helicopter blunt fuselage model was
carried out to evaluate the effectiveness of active flow control (AFC) systems in reducing …

[PDF][PDF] Characterization of the flow around a helicopter fuselage equipped with vortex generators for drag reduction

R Jimenez, F De Gregorio, M Legrand… - … Symposium on the …, 2016 - researchgate.net
The fuselage can be responsible for around 50 to 70% of the total drag of a helicopter. In the
particular case of large transport helicopters with a large flat aft loading ramp, two flow …

[PDF][PDF] Helicopter fuselage drag reduction investigation

F De Gregorio - 17th International symposium on applications of …, 2014 - researchgate.net
The performance of large helicopter transport has been investigated with the aim of reducing
the fuselage drag and increasing the performance. The fuselage drag is responsible of a …

[PDF][PDF] Experimental and numerical investigation of helicopter fuselage model with active flow control

F De Gregorio, PL Vitagliano - 2014 - dspace-erf.nlr.nl
Scope of the work was investigating both experimentally and numerically the flow
characteristics in the wake region of a simplified helicopter fuselage model featuring a rear …

Heavy Class Helicopter Fuselage Model Drag Reduction by Active Flow Control Systems

F De Gregorio - Journal of Physics: Conference Series, 2017 - iopscience.iop.org
A comprehensive experimental investigation of helicopter blunt fuselage drag reduction
using active flow control is being carried out within the European Clean Sky program. The …