Heat transfer performance of aviation kerosene RP-3 flowing in a vertical helical tube at supercritical pressure. (5th July 2017)

• Record Type: Journal Article
• Authors: Wen, Jie; Huang, Haoran; Fu, Yanchen; Xu, Guoqiang; Zhu, Kun
• Is Part Of: Applied thermal engineering. Volume 121(2017)
• Page Start: 853
• Page End: 862
• Publication Date: 2017-07-05
• Subjects: Heat transfer -- Aviation kerosene -- Vertical -- Helical tube -- Supercritical pressure; Heat engineering -- Periodicals; Heating -- Equipment and supplies -- Periodicals; Periodicals; 621.40205
• DOI: 10.1016/j.applthermaleng.2017.04.055
• Languages: English
• ISSNs: 1359-4311

Abstract

Highlights: Buoyancy and centrifugal force effects exist in helical tube at supercritical pressure. Outside HTC is averagely 31.5% larger than the inside at the same cross section. Centrifugal secondary flow plays the key factor to cause heat transfer enhancement at the Richardson ratio φ > 10. Two correlations of Nusselt number are developed based on the experimental data. Abstract: Convective heat transfer characteristics of aviation kerosene RP-3 at supercritical pressure (P = 5 MPa) in vertical helical tube were experimentally studied. The helical tube has 1.82 mm equivalent inner diameter, 20 mm helical diameter and 10 mm pitch. Circumferential temperatures were detected at both upward and downward flow experiments and the results indicated that: The secondary flow induced by centrifugal force moves outward of the cross section and inside temperature is larger than the outside. Thus, the outside heat transfer coefficient (HTC) is averagely 31.5% larger than that of the inside. Furthermore, heat transfer enhancement leading by centrifugal secondary flow is the key factor when the Richardson ratio is larger than 10. At last, two correlations of Nusselt number are developed to predict heat transfer of aviation kerosene RP-3 in helical tube based on experimental data at supercritical pressure.