Novel Aero-Engine Multi-Disciplinary Preliminary Design Optimization Framework Accounting for Dynamic System Operation and Aircraft Mission Performance

This paper presents a modular, flexible, extendable and fast-computational framework that implements a multidisciplinary, varying fidelity, multi-system approach for the conceptual and preliminary design of novel aero-engines. In its current status, the framework includes modules for multi-point ste...

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Detalles Bibliográficos

Principais autores:	Alexios Alexiou, Nikolaos Aretakis, Ioannis Kolias, Konstantinos Mathioudakis
Formato:	Artigo
Idioma:	Inglês
Publicado:	MDPI AG 2021-02-01
Series:	Aerospace
Assuntos:	aero-engine multi-disciplinary control system geared turbofan optimization preliminary design
Acceso en liña:	https://www.mdpi.com/2226-4310/8/2/49
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