Research advances on mist assisted impingement and film cooling of turbine blades-Reference-Cited by-同舟云学术

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Research advances on mist assisted impingement and film cooling of turbine blades

Published:2024-11 Issue: Volume:232 Page:125907
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Biswal Pratibha^ORCID,P. Mallikarjuna Rao,Balaji C.

Publisher

Elsevier BV

Reference146 articles.

1. Review of modern low emissions combustion technologies, for aero gas turbine engines;Liu;Progress Aerosp. Sci.,2017

2. Gas turbine aero-engines real time on-board modelling: A review, research challenges, and exploring the future;Wei;Progress Aerosp. Sci.,2020

3. Exergy as a useful tool for the performance assessment of aircraft gas turbine engines: A key review;Sohret;Prog. Aerosp. Sci.,2016

4. All-electric commercial aviation with solid oxide fuel cell-gas turbine-battery hybrids;Collins;Appl. Energy,2020

5. Use of hot supercritical CO2 produced from a geothermal reservoir to generate electric power in a gas turbine power generation system;Levy. X. Wang C. Pan;J. CO2 Util.,2018

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