Aero-Engine Preliminary Design Optimization and Operability Studies Supported by a Compressor Mean-Line Design Module

Aero-Engine Preliminary Design Optimization and Operability Studies Supported by a Compressor Mean-Line Design Module

An approach for preliminary aero-engine design, incorporating a mean-line code for the design of axial-flow, multi-stage compressors, is presented. The compressor mean-line code is developed and integrated within a framework for the preliminary design and assessment of aero-engine concepts. It is th...

Full description

Bibliographic Details
Main Authors: Alexios Alexiou, Ioannis Kolias, Nikolaos Aretakis, Konstantinos Mathioudakis
Format: Article
Language:English
Published: MDPI AG 2023-08-01
Series:Aerospace
Subjects:
aero-engines
preliminary design
axial compressor
mean-line design
engine optimization
operability
Online Access:https://www.mdpi.com/2226-4310/10/8/726

Similar Items

Similar Items