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Jean  Helder Marques Ribeiro
Jean Helder Marques Ribeiro
Verified email at fem.unicamp.br
Title
Cited by
Cited by
Year
Identification of coherent structures in the flow past a NACA0012 airfoil via proper orthogonal decomposition
JHM Ribeiro, WR Wolf
Physics of Fluids 29 (8), 2017
622017
Randomized resolvent analysis
JHM Ribeiro, CA Yeh, K Taira
Physical Review Fluids 5 (3), 033902, 2020
562020
Analysis of coherent structures in large-eddy simulations of a NACA0012 airfoil
T Rodarte Ricciardi, J Ribeiro, W Wolf
AIAA Scitech 2019 Forum, 0320, 2019
192019
Wing sweep effects on laminar separated flows
JHM Ribeiro, CA Yeh, K Zhang, K Taira
Journal of Fluid Mechanics 950, A23, 2022
122022
Triglobal resolvent analysis of swept-wing wakes
JHM Ribeiro, CA Yeh, K Taira
Journal of Fluid Mechanics 954, A42, 2023
102023
Wake dynamics of tapered wings. Part III: triglobal linear stability analysis
A Burtsev, V Theofilis, JHM Ribeiro, K Taira, J Neal, M Amitay
AIAA SCITECH 2023 Forum, 2299, 2023
62023
Wake dynamics of tapered wings. Part I: a computational study
JHM Ribeiro, K Taira, J Neal, M Amitay, A Burtsev, V Theofilis
AIAA SCITECH 2023 Forum, 2297, 2023
62023
Wake dynamics of tapered wings. Part II: an experimental study
J Neal, B Gares, M Amitay, A Burtsev, V Theofilis, JHM Ribeiro, K Taira
AIAA SCITECH 2023 Forum, 2298, 2023
52023
Sketch-based resolvent analysis
D House, C Skene, JHM Ribeiro, CA Yeh, K Taira
AIAA AVIATION 2022 Forum, 3335, 2022
52022
Laminar post-stall wakes of tapered swept wings
JHM Ribeiro, J Neal, A Burtsev, M Amitay, V Theofilis, K Taira
Journal of Fluid Mechanics 976, A6, 2023
42023
From biglobal to triglobal resolvent analysis: laminar separated flows over swept wings
JHM Ribeiro, CA Yeh, K Zhang, K Taira
AIAA SCITECH 2022 Forum, 2428, 2022
32022
Resolvent-based analysis of low-Reynolds-number separated flows around tapered wings
JHM Ribeiro, K Taira
AIAA AVIATION 2023 Forum, 4354, 2023
22023
Triglobal resolvent-analysis-based control of separated flows around low-aspect-ratio wings
JHM Ribeiro, K Taira
arXiv preprint arXiv:2402.12553, 2024
12024
Similarities in massive separation across Reynolds numbers for swept and tapered finite span wings
J Neal, A Burtsev, JHM Ribeiro, K Taira, V Theofilis, M Amitay
arXiv preprint arXiv:2308.12442, 2023
12023
Numerical analysis of the piston crown geometry influence on the tumble and squish in a single cylinder engine
MGJ Vaz, FGL Amorim, JHM Ribeiro, R Huebner, RM Valle
SAE Technical Paper, 2014
12014
ANÁLISE NUMÉRICA DA TURBULÊNCIA NO ESCOAMENTO DE AR EM MOTOR MONOCILÍNDRICO
JHM Ribeiro
Federal University of Minas Gerais, 2014
12014
An Invitation to Resolvent Analysis
LV Rolandi, JHM Ribeiro, CA Yeh, K Taira
arXiv preprint arXiv:2404.11789, 2024
2024
Direct Numerical Simulations, Resolvent Analysis, and Flow Control of Laminar Post-Stall Wakes Around Finite Tapered Swept Wings
JHM Ribeiro
University of California, Los Angeles, 2023
2023
Laminar flow separation over tapered wings, Part 2: an experimental study
B Gares, J Neal, A Burtsev, J Ribeiro, V Theofilis, K Taira, M Amitay
Bulletin of the American Physical Society 67, 2022
2022
Laminar flow separation over tapered wings, Part 1: a computational study
J Ribeiro, J Neal, A Burtsev, V Theofilis, M Amitay, K Taira
Bulletin of the American Physical Society 67, 2022
2022
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