Review of propulsion technologies for N+ 3 subsonic vehicle concepts

SW Ashcraft, AS Padron, KA Pascioni, GW Stout Jr… - 2011 - ntrs.nasa.gov
NASA has set aggressive fuel burn, noise, and emission reduction goals for a new
generation (N+ 3) of aircraft targeting concepts that could be viable in the 2035 timeframe …

[HTML][HTML] Integration of high-fidelity model of forward variable area bypass injector into zero-dimensional variable cycle engine model

S Fu, Z Li, W Zhanxue, LIN Zhifu, SHI Jingwei - Chinese Journal of …, 2021 - Elsevier
Abstract Forward Variable Area Bypass Injector (FVABI) is one of key components which
contributes to modulate the cycle parameters of Variable Cycle Engine (VCE) under various …

Analysis of discrepancies between 3-D coupled and uncoupled schemes based on CFD in full engine simulation

Y Xu, C Yan, Y Piao - Aerospace Science and Technology, 2022 - Elsevier
Full engine simulations based on three-dimensional computational fluid dynamics (3-D
CFD) allow the visualisation of flow details accompanied by total performances for …

A New Integrated Model for Simulating Adaptive Cycle Engine Performance Considering Variations in Tip Clearance

J Wei, W Zou, Z Song, B Wang, J Li, X Zheng - Processes, 2023 - mdpi.com
The low-fidelity simulation method cannot meet the requirements for predicting the
performance of an adaptive cycle engine (ACE), especially when considering tip clearance …

The Growth Engine Concept and Its Potential for an Electrified Aviation Future

M Kavvalos, KG Kyprianidis… - … of Engineering for …, 2024 - asmedigitalcollection.asme.org
The emerging need for cost-and energy-efficient propulsion systems have shifted the
research interest to radical concepts, with several challenges to overcome in order to enter …

Secondary air system component modeling for engine performance simulations

A Alexiou, K Mathioudakis - 2009 - asmedigitalcollection.asme.org
This paper describes the modeling of typical secondary air system elements such as rotating
orifices, seals, and flow passages with heat and work transfer from the surrounding surfaces …

Turbofan engine health assessment from flight data

N Aretakis, I Roumeliotis… - … for gas turbines …, 2015 - asmedigitalcollection.asme.org
The paper presents the use of different approaches to engine health assessment using on-
wing data obtained over a year from an engine of a commercial short-range aircraft. The on …

Development of a program for transient behavior simulation of heavy-duty gas turbines

JH Kim, TS Kim, SJ Moon - Journal of Mechanical Science and …, 2016 - Springer
In this study, a program for analyzing the transient behaviors of heavy-duty gas turbines was
developed. Focus was given to simulating a practical load-following operation. A distinct …

0D-1D coupled method for performance design and analysis of adaptive cycle engine-Modeling, simulation and validation

W Zou, X Zheng, W Liu, J Lai, B Wang - Energy, 2024 - Elsevier
Adaptive cycle engine (ACE) can efficiently operate in different modes to fulfill complex
mission requirements, which features better mission adaptability than the conventional …

[PDF][PDF] Multi-disciplinary conceptual design of future jet engine systems

KG Kyprianidis - 2010 - researchgate.net
This thesis describes various aspects of the development of a multi-disciplinary aero engine
conceptual design tool, TERA2020 (Techno-economic, Environmental and Risk Assessment …