The application of transpiration cooling as a thermal protection system for hypersonic vehicles (2022)

First Author: Naved I
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/bodleian:xqq6q6gzx

Publication URI: https://ora.ox.ac.uk/objects/uuid:f96e5356-a4d4-449d-a102-9249dbefde3c

Type: Thesis