The response of wall turbulence to streamwise pressure gradients: a computational study

Matthew Brockhaus, Adrian Sescu, Leonardo Chamorro

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

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.

Original languageEnglish (US)
Title of host publicationAIAA Aviation Forum and ASCEND, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624107160
StatePublished - 2024
EventAIAA Aviation Forum and ASCEND, 2024 - Las Vegas, United States
Duration: Jul 29 2024Aug 2 2024

Publication series

NameAIAA Aviation Forum and ASCEND, 2024

Conference

ConferenceAIAA Aviation Forum and ASCEND, 2024
Country/TerritoryUnited States
CityLas Vegas
Period7/29/248/2/24

ASJC Scopus subject areas

  • Energy Engineering and Power Technology
  • Nuclear Energy and Engineering
  • Aerospace Engineering
  • Space and Planetary Science

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