Evolution of a turbulent boundary layer over a series of pressure gradients

Akhileshwar Borra, Theresa Saxton-Fox

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

Abstract

This study investigated the behavior of a turbulent boundary layer over a downward-facing ramp downstream of a flat plate, which imposed spatially varying pressure gradients on the turbulent boundary layer, through time-resolved particle image velocimetry and complementary RANS simulations. The ramp generated a mild favorable pressure gradient (FPG) from the leading edge of the flat plate, a strong FPG directly upstream of the ramp and a strong adverse pressure gradient on the ramp’s surface. The streamwise evolution of the turbulent boundary layer was evaluated using the PIV data, and comparisons between the PIV data and RANS simulations were performed at three different Reynolds numbers. The mean streamwise velocity contours showed a slight acceleration of the boundary layer due to the strong FPG before the ramp. On the ramp’s surface, the boundary layer decelerated significantly under the strong adverse pressure gradient, causing substantial reverse flow. The turbulent boundary layer detached at all Reynolds numbers, with higher Reynolds numbers detaching further downstream. Reynolds stresses increased in magnitude from the first to the fourth streamwise location, then decreased, with wall-normal peak positions shifting away from the wall before recovering beyond x/L = 0.5. Although the patterns were similar across Reynolds numbers, the overall Reynolds stresses decreased with higher Reynolds numbers. Comparisons between experimental data and RANS simulations revealed slight discrepancies in the detachment and reattachment points and the wall-normal extent of mean reverse flow.

Original languageEnglish (US)
Title of host publicationAIAA Aviation Forum and ASCEND, 2024
PublisherAmerican Institute of Aeronautics and Astronautics Inc. (AIAA)
ISBN (Print)9781624107160
DOIs
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

Fingerprint

Dive into the research topics of 'Evolution of a turbulent boundary layer over a series of pressure gradients'. Together they form a unique fingerprint.

Cite this