Experimental and numerical investigation of heat transfer and pressure drop for innovative gas cooled systems

被引:4
|
作者
Gomez, R. [1 ]
Buchholz, S. [2 ]
Suikkanen, H. [3 ]
机构
[1] Karlsruhe Inst Technol, Inst Neutron Phys & Reactor Technol, D-76344 Eggenstein Leopoldshafen, Germany
[2] Gesell Anlagen & Reaktorsicherheit GRS mbH, D-85748 Garching, Germany
[3] Lappeenranta Univ Technol, LUT Energy, FI-53851 Lappeenranta, Finland
关键词
Enhancement mechanism - Gas-cooled fast reactors - Heat transfer and pressure drop - Heat Transfer enhancement - Hexagonal cross-sections - Numerical investigations - Temperature profiles - Transmutation systems;
D O I
10.1016/j.nucengdes.2014.11.010
中图分类号
TL [原子能技术]; O571 [原子核物理学];
学科分类号
0827 ; 082701 ;
摘要
Heat transfer enhancement through turbulence augmentation is recognized as a key factor for improving the safety and economic conditions in the development of both critical and subcritical innovative advanced gas cooled fast reactors (GFR) and transmutation systems. The L-STAR facility has been designed and erected at the Karlsruhe Institute of Technology (KIT) to study turbulent flow behavior and its heat transfer enhancement characteristics in gas cooled annular channels under a wide range of conditions. The test section consists of an annular hexagonal cross section channel with are inner electrical heater rod element, placed concentrically within the test section, which seeks to simulate the flow area of a fuel rod element in a GFR. The long term objective of the experimental study is to investigate and improve the understanding of complex turbulent convective enhancement mechanisms as well as the friction loss penalties of roughened fuel rods compared to smooth ones and to generate an accurate database for further development of physical models. In the first step, experimental results of the fluid flow with uniform heat release conditions for the smooth heater rod are presented. The pressure drops, as well as the axial temperature profiles along the heater rod surface have been measured at Reynolds numbers in the range from 4000 to 35,000. The experimental results of the first stage were compared with independently conducted CFD analyses performed at Lappeenranta University of Technology (LUT) with the code ANSYS Fluent and at Gesellschaft fur Anlagen- und Reaktorsicherheit (GRS) with the code ANSYS CFX. (C) 2014 Elsevier B.V. All rights reserved.
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页码:40 / 50
页数:11
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