|Table of Contents|

Investigation on flow and heat transfer of high temperature and high pressure hydrogen in triangular grooves and tubes(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2020年06期
Page:
35-44
Research Field:
研究与设计
Publishing date:

Info

Title:
Investigation on flow and heat transfer of high temperature and high pressure hydrogen in triangular grooves and tubes
Author(s):
LIU Lin1FANG Yuliang2WU Junmei1WANG Chenglong2MA Yuan3TIAN Wenxi2
(1.State Key Laboratory for Strength and Vibration of Mechanical Structures, Shaanxi Key Laboratory of Environment and Control for Flight Vehicle, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an, 710049, China; 2.State Key Laboratory of Multiphase Flow in Power Engineering, School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an 710049, China; 3.Xi'an Aerospace Propulsion Institute, Xi'an 710100, China)
Keywords:
hydrogen flow and heat transfer triangular groove numerical simulation high temperature and high pressure
PACS:
V439+.5
DOI:
-
Abstract:
Under high temperature and high pressure conditions, the flow and heat transfer characteristics of hydrogen in long straight tubes heated by the uniform heat flux and triangular fluted enhanced tubes were studied by the numerical simulation method.The change of thermophysical properties of hydrogen with temperature and pressure was considered in the simulation, and the SST k-ω turbulence model was adopted.The numerical results of this model are in good agreement with the experimental data in the circular channel of related literature.The results show that the flow of hydrogen in the cooling channel is subsonic turbulence, and the wall temperature of the cooling channel gradually increases along the axial direction and then slightly decreases near the outlet.The triangular groove on the inner wall of the circular tube as the turbulator has an obvious effect on enhancing the heat transfer but increasing the flow resistance.Increasing groove depth, decreasing groove spacing and asymmetric triangular groove reduce the overall heat transfer performance.The enhanced heat transfer performance of the inward triangular fluted enhanced tube is better than that of the outward triangular fluted enhanced tube.

References:

[1] 廖宏图.核热推进技术综述[J].火箭推进,2011,37(4):1-11. LIAO H T.Overview of nuclear thermal propulsion technologies[J].Journal of Rocket Propulsion,2011,37(4):1-11.
[2] 张郁.电推进技术的研究应用现状及其发展趋势[J].火箭推进,2005,31(2):27-36. ZHANG Y.Current status and trend of electric propulsion technology development and application[J].Journal of Rocket Propulsion,2005,31(2):27-36.
[3] 苏著亭,杨继材,柯国土.空间核动力[M].上海: 上海交通大学出版社,2016.
[4] 何伟锋,向红军,蔡国飙.核火箭原理、发展及应用[J].火箭推进,2005,31(2):37-43. HE W F,XIANG H J,CAI G B.The fundamentals,developments and applications of nuclear rocket propulsion[J].Journal of Rocket Propulsion,2005,31(2):37-43.
[5] FITTJE J E.Conceptual engine system design for NERVA derived 66.7KN and 111.2KN thrust nuclear thermal rockets[C]//AIP Conference Proceedings.Albuquerque,New Mexico:AIP,2006.
[6] 廖宏图.空间核动力技术概览与发展脉络初探[J].火箭推进,2016,42(5):58-65. LIAO H T.Survey and venation analysis on space nuclear power[J].Journal of Rocket Propulsion,2016,42(5):58-65.
[7] MCCARTHY J R,WOLF H.Forced convection heat transfer to gaseous hydrogen at high heat flux and high pressure in a smooth,round,electrically heated tube[J].ARS Journal,1960,30(4):423-425.
[8] TAYLOR M F.Experimental local heat-transfer and average friction data for hydrogen and helium flowing in a tube at surface temperatures up to 5600 R[Z].1964.
[9] HESS H L,KUNZ H R.A study of forced convection heat transfer to supercritical hydrogen[J].Journal of Heat Transfer,1965,87(1):41-46.
[10] LYON L L.Performance of(U,Zr)C-graphite(composite)and of(U,Zr)C(carbide)fuel elements in the Nuclear Furnace 1 test reactor[R].Office of Scientific and Technical Information(OSTI),1973.
[11] APPEL B.Multiphysics design and simulation of a tungsten-cermet nuclear thermal rocket[D].Texas: Texas A & M University,2012.
[12] SINGH S B.A numerical study of high temperature and high velocity gaseous hydrogen flow in a cooling channel of a NTR core[D].Texas: University of New Orleans,2013.
[13] AKYUZLU K M.Numerical study of high-temperature and high-velocity gaseous hydrogen flow in a cooling channel of a nuclear thermal rocket core[J].Journal of Nuclear Engineering and Radiation Science,2015,1(4):041006.
[14] 艾青,王帅,吴家欢,等.核热推进冷却通道热工特性影响因素研究[J].工程热物理学报,2018,39(12):2745-2748.
[15] 房玉良,秦浩,王成龙,等.高温、高流速氢气在圆管内流动换热特性研究[J].原子能科学技术,2020,54(10):1762-1770.
[16] GOULD D W,HOFF B W,YOUNG M P,et al.Numerical analysis of a single minichannel within a high-temperature hydrogen heat exchanger for beamed energy propulsion applications[C]//Proceedings of ASME 2013 Heat Transfer Summer Conference.Minneapolis,Minnesota:ASME,2013.
[17] JI Y,SHI L,SUN J.Numerical investigation of convective heat transfer to supercritical hydrogen in a straight tube[C]//Proceedings of 2017 25th International Conference on Nuclear Engineering.Shanghai:[s.n.],2017.
[18] JI Y,SUN J,SHI L.Numerical investigation of convective heat transfer to supercritical pressure hydrogen in a straight tube[J].Journal of Nuclear Engineering and Radiation Science,2018,4(3):031012.
[19] MCCARTY R D,HORD J,RODER H M.Selected properties of hydrogen(engineering design data)[R].NASA-SP-3089,1981.
[20] 林宗虎.强化传热及其工程应用[M].北京: 机械工业出版社,1987.

Memo

Memo:
-
Last Update: 1900-01-01