Transpiration cooling of a hypersonic vehicle (2021)
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.5287/ora-vmnnegqxp
Publication URI: https://ora.ox.ac.uk/objects/uuid:e04ab19f-7605-445e-be68-5927ec5703a5
Type: Thesis