Mauro Minervino
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View article: The Aerodynamic Design of a Compliant Morphing Flap for Next-Generation Hybrid Electric Regional Aircraft
The Aerodynamic Design of a Compliant Morphing Flap for Next-Generation Hybrid Electric Regional Aircraft Open
The focus of this paper is on some of the activities performed by CIRA under the framework of the HERWINGT project (Hybrid Electric Regional Wing Integration Novel Wing Technologies) supported by the Clean Aviation Joint Undertaking and fu…
View article: Experimental and Analytical Evaluation of Low-Noise Propeller Designs for Large Regional Aircraft
Experimental and Analytical Evaluation of Low-Noise Propeller Designs for Large Regional Aircraft Open
International audience
View article: On the spurious effects in Lamb-vector-based force decomposition methods
On the spurious effects in Lamb-vector-based force decomposition methods Open
Recent methods based on Lamb vector integration allow for a far-field formulation and decomposition of the whole aerodynamic force, with identification of local flow structures associated with the force generation. Different exact Lamb-vec…
View article: A unified thermodynamic/Lamb-vector-based analysis of the aerodynamic force
A unified thermodynamic/Lamb-vector-based analysis of the aerodynamic force Open
The Lamb vector, cross-product of flow vorticity and velocity, is at the basis of different far-field methods developed in the last decades for the aerodynamic force analysis and decomposition, as an alternative to the nowadays well-assess…
View article: Drag Reduction by Wingtip-Mounted Propellers in Distributed Propulsion Configurations
Drag Reduction by Wingtip-Mounted Propellers in Distributed Propulsion Configurations Open
Tip-mounted propellers can increase wing aerodynamic efficiency, and the concept is gaining appeal in the context of hybrid electrical propulsion for greener aviation, as smaller and lighter electrical motors can help with mitigating struc…
View article: Active Buffet Control on Wing Trailing Edge
Active Buffet Control on Wing Trailing Edge Open
The presentation Shows the result of a 4 year Research activity on trailing edge buffet control by fluidic Gurneys and micro-circulation-control in the scope of the European Project AFLoNext
View article: Prediction of the acoustic shielding by aircraft empennage for contra-rotating open rotors
Prediction of the acoustic shielding by aircraft empennage for contra-rotating open rotors Open
This paper presents a numerical study of the acoustic shielding of aeroengine noise by the aircraft structure. More specifically, the engines considered are contra-rotating open rotors in pusher mode which are installed at the rear of the …
View article: Comparison of Optimization Strategies for High-Lift Design
Comparison of Optimization Strategies for High-Lift Design Open
The design of high-lift systems represents a challenging task within the aerospace community, being a multidisciplinary, multi-objective, and multipoint problem. The Design, Simulation and Flight Reynolds Number Testing for Advanced High-L…