Transpiration cooling for double-walled jet engine turbine blades (2023)
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-w4qyjkrv2
Publication URI: https://ora.ox.ac.uk/objects/uuid:5ac8f9bc-f0b6-45d2-a377-e16953eae3df
Type: Thesis