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L. Botero-Bolivar
L. Botero-Bolivar
PhD candidate, University of Twente
Verified email at utwente.nl
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Cited by
Cited by
Year
Aerodynamic design analysis of a UAV for superficial research of volcanic environments
PD Bravo-Mosquera, L Botero-Bolivar, D Acevedo-Giraldo, ...
Aerospace Science and Technology 70, 600-614, 2017
642017
Aeroacoustic airfoil shape optimization enhanced by autoencoders
J Kou, L Botero-Bolívar, R Ballano, O Marino, L De Santana, E Valero, ...
Expert Systems with Applications 217, 119513, 2023
212023
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
Parametric analysis of the influence of slat geometry on acoustic noise
L Botero, LT Lima Pereira, D Acevedo, F Catalano, DC Reis, EL Coelho
2018 AIAA/CEAS Aeroacoustics Conference, 3593, 2018
162018
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 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
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
Experimental and Numerical Analysis of the Aerodynamic and Aeroacoustic Properties of a 2D High-Lift Wing Model
LT Lima Pereira, L Botero, MT de Araujo, F Catalano, DC Reis, EL Coelho
2018 AIAA/CEAS Aeroacoustics Conference, 3458, 2018
52018
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
Aerodynamic evaluation of different car carrier devices for drag reduction using CFD
D Acevedo-Giraldo, L Botero-Bolívar, D Munera-Palacio, ...
Journal of Aerospace Technology and Management 10, e4018, 2018
42018
Airfoil Trailing Edge Noise Measurements in an Open-jet, Hard-wall and Kevlar-wall Test Section: a Benchmark Exercise.
MP Sanders, L Botero, LD de Santana, C Venner
AIAA AVIATION 2021 FORUM, 2253, 2021
32021
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
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