## Abstract The present work experimentally investigates the effect of vortex generators, in the form of small tabs projecting normally into the flow at the nozzle exit, on the fluid flow and heat transfer characteristics of an axisymmetric impinging air jet in the subcritical Reynolds number range
Effects of plate temperature on heat transfer and emissions of impinging flames
β Scribed by H.B. Li; H.S. Zhen; C.W. Leung; C.S. Cheung
- Publisher
- Elsevier Science
- Year
- 2010
- Tongue
- English
- Weight
- 729 KB
- Volume
- 53
- Category
- Article
- ISSN
- 0017-9310
No coin nor oath required. For personal study only.
β¦ Synopsis
Experiments were conducted to investigate the heat transfer and CO/NO X emissions of a premixed LPG/ air circular flame jet impinging upwards normally to a flat rectangular plate. Temperatures of the impingement plate were controlled by cooling water at 38 Β°C, 58 Β°C and 78 Β°C which was circulating at its back in order to create different plate temperatures. Under each plate temperature, the effects of Reynolds number (Re), equivalence ratio (U) and nozzle-to-plate distance (H) on the heat transfer and CO/ NO X emissions were examined. The Re was selected to be 500, 1000 and 1500 to ensure laminar flame jets. The values of U were chosen to cover fuel-lean, stoichiometric and fuel-rich conditions. The H varied from 3d to 7d with an interval of 1d.
The flame-side temperature of the impingement plate is enhanced when the cooling water temperature increases, but the temperature difference across the impingement plate is reduced. Heat transfer from the flame to the plate is suppressed at higher cooling water temperature. The heat transfer rate is the highest when the cooling water temperature is at 38 Β°C and the lowest heat flux is obtained at 78 Β°C. At the highest cooling water temperature of 78 Β°C, the CO emission is reduced whereas the NO X emission is enhanced. However, this trend is reversed at the lowest cooling water temperature of 38 Β°C.
π SIMILAR VOLUMES
Several CFD calculations have been performed in order to assess the ability of common __kβΟ΅__ turbulence models to predict heat transfer in impingingβjet flow. One focus is on the influence of the wall on the flow, calculated either by applying a logarithmic wall function or by resolving the flow do