Effects of Upstream Wall Heating on Mixed Convection in Separated Flows
Abstract
Measurements and predictions are reported for buoyancy-assisting, laminar mixed convection boundary-layer flow of air along a two-dimensional, vertical backward-facing step, in which the upstream wall and the step are heated to a uniform temperature while the downstream wall is heated to the same or different uniform temperature. The experiments were performed on a backward-facing step geometry, with a step height of 0.8 cm, over a range of freestream velocities 0.26 ≤ u∞ ≤ 0.41 m/s and a range of temperature differences 0 ≤ ΔT ≤ 34°C between the heated walls and the freestream. Laser Doppler velocimeter and cold-wire anemometer were utilized to measure, respectively, the air velocity and the temperature simultaneously. Flow visualizations were also performed to determine the flow reattachment length behind the backward-facing step. Reported measurements are limited to the case where the upstream wall and the step are heated to the same uniform temperature as the downstream wall, but numerical results are presented for the cases where these two temperatures are different and also for the situation when the upstream wall and the step are maintained as adiabatic surfaces. These results reveal that heating of the upstream wall and the step significantly affects the reattachment length, the velocity and temperature distributions, and the rate of heat transfer downstream of the backward-facing step.
Recommended Citation
H. I. Abu-Mulaweh et al., "Effects of Upstream Wall Heating on Mixed Convection in Separated Flows," Journal of Thermophysics and Heat Transfer, American Institute of Aeronautics and Astronautics (AIAA), Jan 1995.
The definitive version is available at https://doi.org/10.2514/3.729
Department(s)
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
0887-8722
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 1995 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
01 Jan 1995