Document is current

Any future updates will be listed below

An approach to indirect estimation of high pressure turbine inlet temperature of turbofan engines based on gas path thermodynamic relations

Crossref DOI link: https://doi.org/10.1007/s12206-015-1045-6

Published Online: 2015-12-05

Published Print: 2015-11

Update policy: https://doi.org/10.1007/springer_crossmark_policy

About CrossMark