Trailing-edge noise comparability in open, closed, and hybrid wind tunnel test sections MPJ Sanders, CFJ Koenjer, L Botero-Bolivar, FL dos Santos, CH Venner, ... AIAA journal 60 (7), 4053-4067, 2022 | 20 | 2022 |
Modeling the Turbulence Spectrum Dissipation Range for Leading-Edge Noise Prediction FL dos Santos, L Botero-Bolívar, C Venner, LD de Santana AIAA journal 60 (6), 3581-3592, 2022 | 19 | 2022 |
Inflow turbulence distortion for airfoil leading-edge noise prediction for large turbulence length scales for zero-mean loading FL dos Santos, L Botero-Bolívar, CH Venner, LD de Santana The Journal of the Acoustical Society of America 153 (3), 1811-1822, 2023 | 14 | 2023 |
Influence of Roughness Trips on Near-and Far-Field Trailing-Edge Noise FL Dos Santos, L Botero-Bolívar, C Venner, LD de Santana AIAA journal 60 (10), 5880-5889, 2022 | 12 | 2022 |
Influence of tripping devices in hastening transition in a flat plate submitted to zero and favorable pressure gradients FL dos Santos, MP Sanders, L Dantas de Santana, C H. Venner AIAA Scitech 2020 Forum, 0046, 2020 | 12 | 2020 |
Modelling the Dissipation Range of von Kármán Turbulence Spectrum FL Dos Santos, L Botero, C Venner, LD de Santana AIAA AVIATION 2021 FORUM, 2292, 2021 | 11 | 2021 |
The Increase of the Airfoil Trailing Edge Noise and Unsteady Surface Pressure due to High Inflow Turbulence L Botero, FL dos Santos, C Venner, LD de Santana AIAA AVIATION 2021 FORUM, 2234, 2021 | 9 | 2021 |
Increase of Unsteady Pressure at a Trailing Edge due to Inflow Turbulence L Botero-Bolívar, FL dos Santos, CH Venner, L de Santana AIAA Journal 60 (12), 6798-6813, 2022 | 8 | 2022 |
Influence of Surface Roughness Geometry on Trailing Edge Wall Pressure Fluctuations and Noise FL Dos Santos, NA Even, L Botero, C Venner, LD de Santana AIAA AVIATION 2021 FORUM, 2294, 2021 | 8 | 2021 |
Influence of break-in on the leakage through reed-type valves of low-capacity refrigeration compressors FL dos Santos, E Silva, CJ Deschamps International Journal of Refrigeration 108, 138-144, 2019 | 7 | 2019 |
Analysis of the remote microphone probe technique for the determination of turbulence quantities FL dos Santos, L Botero-Bolívar, CH Venner, LD de Santana Applied Acoustics 208, 109387, 2023 | 6 | 2023 |
The Influence of Surface Roughness Geometry on the Trailing Edge Unsteady Pressure and Noise FL dos Santos, NAP Even, L Botero-Bolivar, CH Venner, LD de Santana 2021 AIAA Aviation forum Conference, 2021 | 6 | 2021 |
Influence of the Freestream Turbulence on Wall-Pressure Fluctuations Along an Airfoil Chord L Botero-Bolívar, FL dos Santos, CH Venner, L de Santana AIAA Journal 61 (5), 2309-2313, 2023 | 4 | 2023 |
Identification of boundary layer structures by unsteady surface pressure measurements L Botero, FL dos Santos, E Liptiay, CH Venner, LD de Santana AIAA SCITECH 2022 Forum, 1649, 2022 | 4 | 2022 |
Airfoil Trailing-Edge Noise in an Open-jet, a Hard-wall and a Hybrid Test Section Wind Tunnel: a Benchmark Exercise MP Sanders, C Koenjer, LB Bolivar, FL Dos Santos, CH Venner, ... AIAA Aviation Forum 2021, 2021 | 4 | 2021 |
Influence of wear on leakage through reed-type valves of small reciprocating compressors FL dos Santos, E Silva, CJ Deschamps | 4 | 2018 |
Aerodynamic and aeroacoustic characteristics of the NACA 0008 airfoil FL dos Santos, L Botero-Bolívar, CH Venner, LD de Santana 33rd Congress of the International Council of the Aeronautical Sciences …, 2022 | 3 | 2022 |
Wall-pressure spectra, spanwise correlation, and far-field noise measurements of a NACA 0008 airfoil under uniform and turbulent inflows FL dos Santos, L Botero-Bolívar, CH Venner, LD de Santana Applied Acoustics 211, 109546, 2023 | 2 | 2023 |
Study of the development of a boundary layer using the remote microphone probe technique L Botero-Bolívar, FL dos Santos, CH Venner, LD de Santana Experiments in Fluids 64 (4), 88, 2023 | 2 | 2023 |
On the turbulence distortion effects for airfoil leading-edge noise prediction FL dos Santos, L Botero, C Venner, LD de Santana 28th AIAA/CEAS Aeroacoustics 2022 Conference, 3045, 2022 | 2 | 2022 |