03.1 - Aerodynamics – CFD Methods and Validation
COUPLED HEAT TRANSFER CHARACTERISTICS ON CHEMICALLY REACTING INTERFACE OF HIGH-SPEED AIRCRAFT CONSIDERING WALL INJECTION
Q. You¹, X.-F. Yang¹, L. Zeng¹, Y.-W. Gui¹, Y.-X. Du¹, L. Liu¹, G.-M. Xiao¹; ¹China Aerodynamics Research and Development Center, China
The wall injection/suction phenomena exist in TPS and devices of high-speed aircraft. In this paper, surface injection/suction boundary condition was implemented in the CAPTER code. After verifying the boundary condition, it was applied to the coupling modeling of chemically reacting interface in order to predict and research the influence of injection phenomena more accurately and effectively.