Abstract
This article deals with the conceptual approach to optimize efficiency and power of a highly loaded gas turbine flow path design. Different problems were analyzed during low pressure turbine (LPT) preliminary design of high-bypass aircraft jet engine. © 2008 Gas Turbine Society of Japan.
Cite
CITATION STYLE
APA
Romanenko, L., Moroz, L., Pagur, P., Govoruschenko, Y., Spano, E., & Bertini, F. (2008). Advanced gas turbine concept, design and evaluation methodology. Preliminary design of highly loaded low pressure gas turbine of aircraft engine. In International Journal of Gas Turbine, Propulsion and Power Systems (Vol. 2, pp. 17–23). https://doi.org/10.38036/jgpp.2.1_17
Register to see more suggestions
Mendeley helps you to discover research relevant for your work.
Already have an account? Sign in
Sign up for free