Temperature field on flow and heat transfer process for composite nozzle was simulated based on fluid-structure coupled method.While the interface program of computational fluid dynamics (CFD) and finite element method (FEM) were complied
the temperature load and mechanical data transfer was realized rapidly.Then a strategy of thermo-structure coupled computation for composite nozzle was put forward.Direct constraint procedure solved the boundary nonlinear problem caused by carbonization of component interfaces under high temperature.The results show that temperature field computation by coupled method is reasonable and the boundary nonlinear problem has strong influence on the deformation character and stress fields.
Analysis of thermal characteristics of oil⁃cooled aviation wet friction clutch
Calculation of airfoil anti-icing/deicing characteristics based on water film flow and coupled heat transfer
Thermal characteristics for bearing combined EHL theory with CFD method
Fretting wear of discontinuous interface considering centrifugal force and thermal stress
Study on thermometry of leading edge of rotating turbine blade by thermochromic liquid crystal
Related Author
Heyun BAO
Weidi KONG
Wuzhong TAN
Wei HUANG
Rupeng ZHU
XIN Miao
ZHONG Guo
CAO Yihua
Related Institution
National Key Laboratory of Science and Technology on Helicopter Transmission,Hunan Aviation Powerplant Research Institute,Aero Engine Corporation of China
National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics
School of Aeronautic Science and Engineering, ,Beijing University of Aeronautics and Astronautics