TY - GEN
T1 - The response of wall turbulence to streamwise pressure gradients
T2 - AIAA Aviation Forum and ASCEND, 2024
AU - Brockhaus, Matthew
AU - Sescu, Adrian
AU - Chamorro, Leonardo
N1 - Publisher Copyright:
© 2024, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2024
Y1 - 2024
N2 - The effect of pressure gradients on boundary layer flows, whether laminar or turbulent, is a topic of fundamental importance in fluid engineering. Streamwise pressure gradient effects on turbulent boundary layers represent an area that has not been fully explored, and can open a new realm of insights contributing to the understanding of non-equilibrium turbulent flows. In this paper, we will report results from direct numerical simulations of the response of wall turbulence to both adverse and favorable pressure gradients. Dynamic mode decomposition and conventional statistical tools are the main tools that are utilized to analyze the results. By targeting a range of pressure gradient intensities, we quantify the effect that pressure gradients can have on various turbulent statistics and turbulent flow structures.
AB - The effect of pressure gradients on boundary layer flows, whether laminar or turbulent, is a topic of fundamental importance in fluid engineering. Streamwise pressure gradient effects on turbulent boundary layers represent an area that has not been fully explored, and can open a new realm of insights contributing to the understanding of non-equilibrium turbulent flows. In this paper, we will report results from direct numerical simulations of the response of wall turbulence to both adverse and favorable pressure gradients. Dynamic mode decomposition and conventional statistical tools are the main tools that are utilized to analyze the results. By targeting a range of pressure gradient intensities, we quantify the effect that pressure gradients can have on various turbulent statistics and turbulent flow structures.
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M3 - Conference contribution
AN - SCOPUS:85203603264
SN - 9781624107160
T3 - AIAA Aviation Forum and ASCEND, 2024
BT - AIAA Aviation Forum and ASCEND, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
Y2 - 29 July 2024 through 2 August 2024
ER -