A review of installation effects of ultra-high bypass ratio engines

A Magrini, E Benini, HD Yao, J Postma… - Progress in Aerospace …, 2020 - Elsevier
The adoption of ultra-high bypass ratio (UHBPR) engines has been long recognised to bring
about reduction of specific fuel consumption and noise emission. In the need to fulfil …

[HTML][HTML] A review of novel and non-conventional propulsion integrations for next-generation aircraft

K Abu Salem, G Palaia, PD Bravo-Mosquera… - Designs, 2024 - mdpi.com
The aim of this review paper is to collect and discuss the most relevant and updated
contributions in the literature regarding studies on new or non-conventional technologies for …

Layerwise anomaly detection in laser powder-bed fusion metal additive manufacturing

M Mahmoudi, AA Ezzat… - Journal of …, 2019 - asmedigitalcollection.asme.org
A growing research trend in additive manufacturing (AM) calls for layerwise anomaly
detection as a step toward enabling real-time process control, in contrast to ex situ or …

Analysis of fan stage conceptual design attributes for boundary layer ingestion

DK Hall, EM Greitzer, CS Tan - Journal of …, 2017 - asmedigitalcollection.asme.org
This paper describes a new conceptual framework for three-dimensional turbomachinery
flow analysis and its use to assess fan stage attributes for mitigating adverse effects of inlet …

Non-axisymmetric aero-engine nacelle design by surrogate-based methods

F Tejero, R Christie, D MacManus, C Sheaf - Aerospace Science and …, 2021 - Elsevier
For many aerodynamic design tasks, a key challenge is the balance between the non-
linearity of the transonic flow, the inherent 3D nature of the geometry and flow field, the …

Design, aerodynamic analysis and optimization of a next-generation commercial airliner

PD Bravo-Mosquera, HD Cerón-Muñoz… - Journal of the Brazilian …, 2022 - Springer
Unconventional configurations and innovative propulsion technologies have been
continuously developed for reducing both fuel-burn and global net carbon emissions. This …

Impact of Installation on the Performance of a Civil Turbofan Exhaust at Wind-Milling: A Combined Experimental and Numerical Approach

I Goulos, D MacManus, JH Rebassa, J Alderman… - Aerospace Science and …, 2024 - Elsevier
This work presents a combined experimental and numerical investigation of the effect of
wing integration on the aerodynamic behaviour of a typical large civil aero-engine exhaust …

Uhbr open-test-case fan ecl5/catana

V Pagès, P Duquesne, S Aubert, L Blanc… - International Journal of …, 2022 - mdpi.com
The application of composite fans enables disruptive design possibilities but increases
sensitivity to multi-physical resonance between aerodynamic, structure dynamic and …

An automated approach to nacelle parameterization using intuitive class shape transformation curves

R Christie, A Heidebrecht… - … of Engineering for …, 2017 - asmedigitalcollection.asme.org
A tool to create parametric aerodynamic shapes using intuitive design variables based on
class shape transformation (CST) curves is presented. To enable this, a system has been …

Multi-objective optimisation of short nacelles for high bypass ratio engines

F Tejero, M Robinson, DG MacManus… - Aerospace Science and …, 2019 - Elsevier
Future turbo-fan engines are expected to operate at low specific thrust with high bypass
ratios to improve propulsive efficiency. Typically, this can result in an increase in fan …