Heat transfer mechanism of cross-type multi-stream plate-fin heat exchanger (MPFHE) was analyzed and the mathematical model by finite volume method was established based on the research of parallel-counter type MPFHE
and then the distance between fins was separated with cell size by reasonable assumption
expanding the application of former mathematical model. Besides
discussion about choice of cell size was conducted for the airborne cross-type three-stream plate-fin heat exchanger; while the analysis of transverse heat transfer of flow within a cell on the same channel was applied to demonstrate the possibility of ignoring the transverse heat transfer in this direction
so as to increase calculation efficiency under the constant computational accuracy; moreover
experiment of different inlet flow rates or temperatures was carried out to verify the veracity of numerical method. The calculation uncertainty is less than 7.9% compared with the test record
Effect of chamber structure on fuel regression rate and performance of hybrid rocket motor
Two-phase flow numerical calculation of HO/HTPB hybrid rocket engine with diaphragm in grain
Numerical calculation of dynamic performance of low-bypass ratio turbofan engine
Effects of combustion heating vitiated air on kerosene-fueled scramjet performance
Numerical simulation of liquid film and regenerative cooling in a rocket combustor
Related Author
CAI Guo-biao
TIAN Hui
RAO Da-lin
WANG Peng-fei
YU Nan-jia
PENG Sheng-hong
QIAO Wei-yang
TIAN Jin-hu
Related Institution
School of Astronautics, Beijing University of Aeronautics and Astronautics
Aviation Key Laboratory of Science and Technology on Aero-engine Altitude Simulating, China Gas Turbine Establishment, Aviation Industry Corporation of China, Jiangyou Sichuan
School of Power and Energy,Northwestern Polytechnical University
Research Center of Small Sample Technology, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics