Next Article in Journal
The Influence of Combustor Swirl on Pressure Losses and the Propagation of Coolant Flows at the Large Scale Turbine Rig (LSTR): Experimental and Numerical Investigation
Previous Article in Journal
Adjoint-Based Design Optimisation of an Internal Cooling Channel U-Bend for Minimised Pressure Losses
 
 
Article

Article Versions Notes

Int. J. Turbomach. Propuls. Power 2017, 2(3), 11; https://doi.org/10.3390/ijtpp2030011
Action Date Notes Link
article pdf uploaded. 24 June 2017 13:02 CEST Version of Record https://www.mdpi.com/2504-186X/2/3/11/pdf
article xml uploaded. 24 June 2017 13:02 CEST Original file https://www.mdpi.com/2504-186X/2/3/11/xml
article html file updated 24 June 2017 13:04 CEST Original file -
article html file updated 3 May 2019 15:51 CEST Update -
article html file updated 25 September 2019 12:58 CEST Update -
article html file updated 8 February 2020 09:08 CET Update https://www.mdpi.com/2504-186X/2/3/11/html
Back to TopTop