Modeling of Heat Transfer in Microchannel Gas Flow

Author:

Lewandowski Tomasz1,Ochrymiuk Tomasz1,Czerwinska Justyna2

Affiliation:

1. Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-952 Gdansk, Poland

2. Artorg Center, University of Bern, Stauffacherstrasse 78, CH-3014 Bern, Switzerland

Abstract

Due to the existence of a velocity slip and temperature jump on the solid walls, the heat transfer in microchannels significantly differs from the one in the macroscale. In our research, we have focused on the pressure driven gas flows in a simple finite microchannel geometry, with an entrance and an outlet, for low Reynolds (Re<200) and low Knudsen (Kn<0.01) numbers. For such a regime, the slip induced phenomena are strongly connected with the viscous effects. As a result, heat transfer is also significantly altered. For the optimization of flow conditions, we have investigated various temperature gradient configurations, additionally changing Reynolds and Knudsen numbers. The entrance effects, slip flow, and temperature jump lead to complex relations between flow behavior and heat transfer. We have shown that slip effects are generally insignificant for flow behavior. However, two configuration setups (hot wall cold gas and cold wall hot gas) are affected by slip in distinguishably different ways. For the first one, which concerns turbomachinery, the mass flow rate can increase by about 1% in relation to the no-slip case, depending on the wall-gas temperature difference. Heat transfer is more significantly altered. The Nusselt number between slip and no-slip cases at the outlet of the microchannel is increased by about 10%.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference40 articles.

1. Gas Turbine Heat Transfer: Ten Remaining Hot Gas Path Challenges;Bunker;ASME J. Turbomach.

2. Effect of Weak Swirling Flow on Film Cooling Performance;Gau;ASME J. Turbomach.

3. Micro Film Cooling Performance;Li;Int. J. Heat Mass Transfer

4. Film Cooling Effectiveness for Short Film Cooling Holes Fed by a Narrow Plenum;Hale;ASME J. Turbomach.

5. Spatial Arrangement Dependence of Cooling Performance of an Integrated Impingement and Pin Fin Cooling Configuration;Nakamata

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