RANS computations are performed for M∞ = 8.2, Re∞/m = 9.35 × 106 flow past a flat surface with protuberance of size of the same order as that of the boundary layer. The local intensification of heat transfer rates in the vicinity of the protuberance is considered as the main focus of the study. The effect of separated and unseparated boundary layer is considered by varying the protuberance angle. The results are compared with available experimental data. The maximum heat transfer rate, a major design parameter, is found to be fairly predicted by computations. However, accurate prediction of parameters such as upstream separation length and heat flux distribution requires further research and calibration of available turbulence models.
RANS Computations of Hypersonic Interference Heating on Flat Surface with Protuberances
Lect.Notes Mechanical Engineering
Design and Development of Aerospace Vehicles and Propulsion Systems ; Chapter : 17 ; 227-238
2021-03-19
12 pages
Article/Chapter (Book)
Electronic Resource
English
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