Study of turbulent heat transfer of aviation kerosene flows in a curved pipe at supercritical pressure


Autoria(s): Li XF; 仲峰泉; 范学军; Huai XL; Cai J
Data(s)

2010

Resumo

The now and heat transfer characteristics of China No. 3 aviation kerosene in a heated curved tube under supercritical pressure are numerically investigated by a finite volume method. A two-layer turbulence model, consisting of the RNG k-epsilon two-equation model and the Wolfstein one-equation model, is used for the simulation of turbulence. A 10-species kerosene surrogate model and the NIST Supertrapp software are applied to obtain the thermophysical and transport properties of the kerosene at various temperature under a supercritical pressure of 4 MPa. The large variation of thermophysical properties of the kerosene at the supercritical pressure make the flow and heat transfer more complicated, especially under the effects of buoyancy and centrifugal force. The centrifugal force enhances the heat transfer, but also increases the friction factors. The rise of the velocity caused by the variation of the density does not enhance the effects of the centrifugal force when the curvature ratios are less than 0.05. On the contrary, the variation of the density increases the effects of the buoyancy. (C) 2010 Elsevier Ltd. All rights reserved.

Chinese National key Foundation [G2010CB227302]

National Natural Science Foundation of China [50776087, 10672169]

Identificador

http://dspace.imech.ac.cn/handle/311007/43559

http://www.irgrid.ac.cn/handle/1471x/124566

Idioma(s)

英语

Fonte

APPLIED THERMAL ENGINEERING.2010,30(13):1845-1851

Tipo

期刊论文