Advanced Gas Turbine Concept, Design and Evaluation Methodology. Preliminary Design of Highly Loaded Low Pressure Gas Turbine of Aircraft Engine

Leonid Romanenko; Leonid Moroz; Petr Pagur; Yuri Govoruschenko; Ennio Spano; Francesco Bertini

doi:10.38036/jgpp.2.1_17

Leonid Romanenko, Leonid Moroz, Petr Pagur, Yuri Govoruschenko, Ennio Spano, Francesco Bertini

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JOURNAL FREE ACCESS

2008 Volume 2 Issue 1 Pages 17-23

DOI https://doi.org/10.38036/jgpp.2.1_17

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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.

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