Abstract：With the heat transfer characteristics and mechanical properties of various parts of the nozzle, and the particle phase considered, the thermal deformation variation of the nozzle at high temperatures is analyzed in the paper. The results show that the structure of the nozzle has a great influence on the temperature at the fluid-solid interface and the internal interface; the total deformation and the axial deformation of the nozzle are gradually increased along the axial direction, and the value maximizes at the tail, the radial deformation increases first, then decreases and increases again along the axial direction and reaches the maximum at the tail; the twophase flow has a great influence on the deformation of the nozzle, which is an increase in the deformation.
李煜, 程广益, 李宗阳, 窦怡彬, 蒋君庭. 固体火箭发动机喷管两相流动下的热固耦合研究[J]. 空天防御, 2020, 3(1): 1-9.
LI Yu, CHENG Guangyi, LI Zongyang, DOU Yibin, JIANG Junting. Thermo-solid Coupling Study of Solid Rocket Motor Nozzle Under Two-phase Flow. Air & Space Defense, 2020, 3(1): 1-9.
