Follow
Fernanda Leticia dos Santos
Fernanda Leticia dos Santos
Researcher at MARIN
Verified email at marin.nl
Title
Cited by
Cited by
Year
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
182022
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
182022
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
132023
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
122020
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
112022
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
112021
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
92021
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
72022
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
72021
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
72019
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
62023
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
62021
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
42023
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
42022
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
42021
Influence of wear on leakage through reed-type valves of small reciprocating compressors
FL dos Santos, E Silva, CJ Deschamps
32018
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
22023
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
22023
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
22022
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
22022
The system can't perform the operation now. Try again later.
Articles 1–20