Statistics of turbulent boundary layers developing under different pressure gradients

• Grant number: 22/00256-4
• Support Opportunities: Scholarships in Brazil - Master
• Start date: March 01, 2022
• End date: July 31, 2024
• Field of knowledge: Engineering - Aerospace Engineering - Aerodynamics
• Principal Investigator: William Roberto Wolf
• Grantee: Leandro Júnio de Oliveira Silva
• Host Institution: Faculdade de Engenharia Mecânica (FEM). Universidade Estadual de Campinas (UNICAMP). Campinas , SP, Brazil
• Associated research grant: 13/08293-7 - CCES - Center for Computational Engineering and Sciences, AP.CEPID
• Associated scholarship(s): 23/01657-5 - Study of adverse pressure gradient effects in turbulent boundary layers, BE.EP.MS

Abstract

Turbulent boundary layers occur in most flows with industrial applications and in nature, and they usually develop under pressure gradients which modify their stability and turbulence properties. For example, boundary layers on aircraft wings, industrial rotors, and wind and gas turbines are subject to regions of favorable and adverse pressure gradients, the latter being more susceptible to separation. In this work, we will perform wall-resolved large eddy simulations (LES) to analyze the statistics of turbulent boundary layers. Different cambered airfoil profiles will be analyzed to understand the effects of varying adverse pressure gradients on the flow statistics. Tripped boundary layers will be analyzed for a range of subsonic Mach numbers at moderate Reynolds numbers. A study of anisotropy will be conducted through analysis of the Lumley triangle, Reynolds stress anisotropy tensor, scatter plots of velocity components and probability density functions. The role of pressure gradient will be assessed in terms of budgets of turbulent kinetic energy and flow modal decomposition techniques will be employed to extract coherent turbulent structures in the flow. The importance of these organized structures will be investigated on the turbulence statistics.

Scientific publications

(The scientific publications listed on this page originate from the Web of Science or SciELO databases. Their authors have cited FAPESP grant or fellowship project numbers awarded to Principal Investigators or Fellowship Recipients, whether or not they are among the authors. This information is collected automatically and retrieved directly from those bibliometric databases.)

DE O SILVA, LEANDRO JUNI; WOLF, WILLIAM R.; VINUESA, RICARDO. Adverse-pressure-gradient effects on extreme events and intermittency in the turbulent boundary layer of a NACA0012 at 12° angle of attack. AIAA AVIATION FORUM AND ASCEND 2024, v. N/A, p. 13-pg., 2024-01-01. (13/08293-7, 22/00256-4, 21/06448-0, 23/01657-5)

SILVA, LEANDRO J.; WOLF, WILLIAM R.. Pressure gradient effects on coherent structures and anisotropy of a turbulent boundary layer over a NACA0012 airfoil at 12° angle of attack. AIAA AVIATION FORUM AND ASCEND 2024, v. N/A, p. 9-pg., 2024-01-01. (13/08293-7, 22/00256-4, 21/06448-0)

SILVA, LEANDRO JUNIO DE O.; WOLF, WILLIAM R.. Analysis of adverse pressure gradient effects in the boundary layer of a NACA0012 airfoil at high angle of attack. AIAA AVIATION 2023 FORUM, v. N/A, p. 11-pg., 2023-01-01. (13/08293-7, 22/00256-4, 21/06448-0)

Academic Publications

(References retrieved automatically from State of São Paulo Research Institutions)

SILVA, Leandro Júnio de Oliveira. Análise dos efeitos do gradiente de pressão adverso na camada limite turbulenta de um aerofólio NACA0012 em altos ângulos de ataque. 2024. Master's Dissertation - Universidade Estadual de Campinas (UNICAMP). Faculdade de Engenharia Mecânica Campinas, SP.