Daniel Sampaio Souza

CV Lattes ResearcherID ORCID Google Scholar Citations

Universidade Estadual Paulista (UNESP). Campus Experimental São João da Boa Vista. Faculdade de Engenharia (Institutional affiliation from the last research proposal)
Birthplace: Brazil

Graduated in Mechanical Engineering from Federal University of Bahia (UFBA) in 2009, obtained his title of Doctor in Science also in Mechanical Engineering from University of São Paulo (USP) in 2016. Currently Professor of the Aeronautical Engineering Department at São Paulo State University (UNESP). Performs research on Aerodynamics, Turbulence and Aeroacoustics, with experiences in the topics of slat noise and high angle of attack aerodynamics. (Source: Lattes Curriculum)

News published in Agência FAPESP Newsletter about the researcher

More items Less items

TITULO

Articles published in other media outlets ( ):

More items Less items

VEICULO: TITULO (DATA)

Research grants

Ongoing (most recent)

Abstract
The aerodynamic response of inboard sections of rotating wings often diverges from the one expected for the corresponding airfoil in two-dimensional motion with the same angle of attack and Reynolds number. The effects of the apparent forces, centrifugal and Coriolis', and the radial pressure gradient increase the lift generation capability of the section. This increase, frequently referr…
Investigation of the rotational effect on the separate flow over sections of wind turbines: coherent structures and rotational augmentation, AP.R

Completed (most recent)

Scholarships in Brazil

Completed (most recent)

Abstract
The dynamic stall is responsible for a significant excess of aerodynamic load on wind-turbine and helicopter blades. Such high dynamical load may cause the failure of these systems through fatigue. Semi-empirical dynamic stall models are widely used both for blade design and investigations of their structural behavior. Therefore, improvements of these models are of fundamental importance …
Comparison between RANS simulations and assumptions adopted by a semi-empirical dynamic stall model, BP.IC
Abstract
The blade element momentum (BEM) method is an aerodynamic tool widely used for the analysis and design of horizontal axis wind turbines.The method demands as input polar curves for the airfoils of the blade sections. These curves are commonly obtained through wind tunnel measurements or two-dimensional simulations. Since it neglects rotational effects, in its original formulation, the BEM…
Use of quasi-3D CFD simulations to generate polar curves for blade element momentum computations, BP.IC

Virtual Library in numbers * Updated data on July 19, 2025

Total / Available in English

1 / 1	Ongoing grants
2 / 2	Completed research grants
2 / 2	Completed scholarships in Brazil
5 / 5	All research grants and scholarships

Associated processes

Most frequent collaborators in research granted by FAPESP

Keywords used by the researcher

Aerospace Engineering Engineering Mechanical Engineering

Please report errors on the page using this form.

Short URL

Abstract

Abstract

Abstract