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Ioannis Templalexis

Researcher at Hellenic Air Force Academy

Publications -  25
Citations -  240

Ioannis Templalexis is an academic researcher from Hellenic Air Force Academy. The author has contributed to research in topics: Gas compressor & Axial compressor. The author has an hindex of 9, co-authored 25 publications receiving 220 citations.

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Journal ArticleDOI

Towards a full two dimensional gas turbine performance simulator

TL;DR: In this paper, the full integration of two-dimensional streamline curvature component models with a low-fidelity cycle program is presented, along with the effect of three different intake lip geometry on the performance of a notional, two-spool, low-bypass ratio, military engine.
Journal ArticleDOI

A Fully Integrated Approach to Component Zooming Using Computational Fluid Dynamics

TL;DR: In this article, the performance characteristics of an isolated gas turbine engine component, resolved from a detailed, high-fidelity analysis, is transferred to an engine system analysis carried out at a lower level of resolution.
Journal ArticleDOI

A comparison of component zooming simulation strategies using streamline curvature

TL;DR: In this paper, a direct comparison of three well-established zooming strategies utilizing a two-dimensional streamline curvature component model is presented. But the results of the comparison are limited to the case where real component characteristics are not available.
Proceedings ArticleDOI

Development of a 2-D Compressor Streamline Curvature Code

TL;DR: The Streamline Curvature (SLC) software as discussed by the authors is a two-dimensional flow simulation software that can be used to analyze the flow inside a compressor in two dimensions.
Journal ArticleDOI

Prediction of Engine Performance Under Compressor Inlet Flow Distortion Using Streamline Curvature

TL;DR: In this paper, a two-dimensional, streamline curvature compressor software is used to simulate the characteristics of any compressor at several operating conditions and is subsequently used in the zero-dimensional cycle analysis to provide a more accurate, physics-based estimate of compressor performance under clean and distorted inlet conditions, replacing the default compressor maps.