activity
20192022
most citedTransition, intermittency and phase interference effects in airfoil secondary tones and acoustic feedback loop

50 citations · 105 across the 4 of their papers we have counts for

collaborators

5 papers

physics.flu-dyn2022★ 28 cited

Switch of tonal noise generation mechanisms in airfoil transitional flows

Tulio R. Ricciardi, William R. Wolf

Large eddy simulations are performed to study tonal noise generation by a NACA0012 airfoil at an angle of attack deg. and freestream Mach number of . D…

physics.flu-dyn2022★ 26 cited

Unsteadiness of Shock-Boundary Layer Interactions in a Mach 2.0 Supersonic Turbine Cascade

Hugo F. S. Lui, Tulio R. Ricciardi, William R. Wolf +3

The physics of shock-boundary layer interactions (SBLIs) in a supersonic turbine cascade at Mach 2.0 and Reynolds number 395,000, based on the axial chord, is investigated through…

physics.flu-dyn2021★ 1 cited

On the application of incomplete FWH surfaces for aeroacoustic predictions

Tulio Ricciardi, William Wolf, Philippe Spalart

This work is motivated by CFD simulations from a realistic landing gear performed modeling only the half bottom of the aircraft fuselage [15]. Hence, in this previous analysis, the…

physics.flu-dyn2021★ 50 cited

Transition, intermittency and phase interference effects in airfoil secondary tones and acoustic feedback loop

Tulio R. Ricciardi, William R. Wolf, Kunihiko Taira

A large eddy simulation is performed to study secondary tones generated by a NACA0012 airfoil at angle of attack of with freestream Mach number of …

physics.flu-dyn2019

On Secondary Tones Arising in Trailing-Edge Noise at Moderate Reynolds Numbers

Tulio R. Ricciardi, Walter Arias-Ramirez, William R. Wolf

Direct numerical simulations are carried out to investigate the flow features responsible for secondary tones arising in trailing-edge noise at moderate Reynolds numbers. Simulatio…