Modelling hypersonic flows in thermochemical nonequilibrium using adaptive mesh refinement (2020)
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Publication URI: https://api.elsevier.com/content/abstract/scopus_id/85081053761
Type: Other
Parent Publication: Proceedings of the 6th European Conference on Computational Mechanics: Solids, Structures and Coupled Problems, ECCM 2018 and 7th European Conference on Computational Fluid Dynamics, ECFD 2018