Nowadays the majority of civil aircraft employs swept-back wings. This configuration, proposed in the early 30s of last century, has been technologically motivated by the otherwise enhanced drag experienced in transonic cruise condition
An experimental study was carried out to understand the way the turbulence interacts with the bounda...
We reveal the effects of sweep on the wake dynamics around NACA 0015 wings at high angles of attack ...
PhDA study has been carried out of the aerodynamic interference flow arising at the junction of a s...
Due to the presence of a singularity in the governing three-dimensional (3D) momentum integral equat...
A high level of turbulence is generated in the region upstream of the leading edge of a wing. The ph...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
Due to a singularity in the governing three-dimensional turbulent momentum integral equations at the...
Experimental investigations were performed to elucidate the features of flow fields occurring over c...
Wing sweep has been studied by industry and academia since the pioneering days of aviation for both ...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...
An experimental study, based on a swept wing, was undertaken in the water tunnel and the wind tunnel...
This article uses triglobal stability analysis to address the question of shock-buffet unsteadiness,...
Large Eddy Simulation (LES) was used to model the formation of a crossflow vortex packet in a 3-dime...
Abstract-The transonic area rule was first implemented in the 1950s. It is an important concept rela...
Flight tests on the Handley Page suction wing showed that turbulence, generated at the wing root, c...
An experimental study was carried out to understand the way the turbulence interacts with the bounda...
We reveal the effects of sweep on the wake dynamics around NACA 0015 wings at high angles of attack ...
PhDA study has been carried out of the aerodynamic interference flow arising at the junction of a s...
Due to the presence of a singularity in the governing three-dimensional (3D) momentum integral equat...
A high level of turbulence is generated in the region upstream of the leading edge of a wing. The ph...
The work contained in this report is concerned with the use of transpiration at the leading edge of ...
Due to a singularity in the governing three-dimensional turbulent momentum integral equations at the...
Experimental investigations were performed to elucidate the features of flow fields occurring over c...
Wing sweep has been studied by industry and academia since the pioneering days of aviation for both ...
This work is motivated by the need for low-order aerodynamic models to predict accurately the effect...
An experimental study, based on a swept wing, was undertaken in the water tunnel and the wind tunnel...
This article uses triglobal stability analysis to address the question of shock-buffet unsteadiness,...
Large Eddy Simulation (LES) was used to model the formation of a crossflow vortex packet in a 3-dime...
Abstract-The transonic area rule was first implemented in the 1950s. It is an important concept rela...
Flight tests on the Handley Page suction wing showed that turbulence, generated at the wing root, c...
An experimental study was carried out to understand the way the turbulence interacts with the bounda...
We reveal the effects of sweep on the wake dynamics around NACA 0015 wings at high angles of attack ...
PhDA study has been carried out of the aerodynamic interference flow arising at the junction of a s...
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