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

A Alexiou, N Aretakis, I Kolias, K Mathioudakis - Aerospace, 2021 - mdpi.com
This paper presents a modular, flexible, extendable and fast-computational framework that
implements a multidisciplinary, varying fidelity, multi-system approach for the conceptual …

[HTML][HTML] An efficient multi-fidelity simulation approach for performance prediction of adaptive cycle engines

W Zou, Z Song, B Wang, M Wen… - Journal of the Global …, 2024 - journal.gpps.global
Adaptive cycle engine (ACE) with multi-stream, modulated bypass ratio, and high-thrust/high-
efficiency mode provides the capability of multiple mission adaptation for the next …

Automated component preliminary design and evaluation in the overall engine using fully coupled approaches

J Schmeink, M Schnoes - … Expo: Power for …, 2022 - asmedigitalcollection.asme.org
Engine development is a long and complex process. Errors or unfavorable decisions made
in the preliminary design phase have a lasting negative impact on the entire development …

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

A Alexiou, I Kolias, N Aretakis, K Mathioudakis - Aerospace, 2023 - mdpi.com
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 …

A Tool for the Design of Turbomachinery Disks for an Aero-Engine Preliminary Design Framework

I Kolias, N Aretakis, A Alexiou, K Mathioudakis - Aerospace, 2023 - mdpi.com
Disks in gas turbines are optimized for minimum weight, while satisfying both geometry and
stress constraints, in order to minimize the engine production, operation, and maintenance …

1D multi-point marine turbocharger design, for optimal performance recovery

K Ntonas, N Aretakis, OA Koskoletos… - Proceedings of the …, 2023 - journals.sagepub.com
An integrated turbocharger 1D design tool, allowing retrofit of both compressor and turbine
is presented. An optimization procedure is employed, to design both compressor and turbine …

Performance prediction of transonic axial multistage compressor based on one-dimensional meanline method

Y Zhang, S Zhang - … Engineers, Part A: Journal of Power and …, 2021 - journals.sagepub.com
This study proposes a 1D meanline program for the modeling of modern transonic axial
multistage compressors. In this method, an improved blockage factor model is proposed …

An improved method of one-dimensional meanline model for axial flow compressor performance prediction

W Sun, W Wang, T He, W He, J Hu - IET Conference Proceedings CP894, 2024 - IET
One-dimensional methods have the advantage of fast computation and convergence in
predicting the performance of axial flow compressors. However, the empirical models used …

[PDF][PDF] Tool for the Design of Turbomachinery Disks for an Aero-Engine Preliminary Design Framework. Aerospace 2023, 10, 460

I Kolias, N Aretakis, A Alexiou, KA Mathioudakis - 2023 - academia.edu
Disks in gas turbines are optimized for minimum weight, while satisfying both geometry and
stress constraints, in order to minimize the engine production, operation, and maintenance …

Разработки математической модели и компьютерной программы первичного проектирования трансзвуковых осевых компрессоров

АИ Боровков, ЮБ Галеркин… - ОМСКИЙ НАУЧНЫЙ …, 2020 - cyberleninka.ru
В работе представлена математическая модель, лежащая в основе программы
расчета и проектирования осевых компрессоров. Описан процесс расчета потерь …