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 …

A review of helicopter rotor blade tip shapes

A Brocklehurst, GN Barakos - Progress in aerospace sciences, 2013 - Elsevier
A review of helicopter rotor blade tip design technology has been carried out with a view to
undertaking subsequent computations to evaluate the performance of new tip designs. The …

Drag/thrust analysis of jet-propelled transonic transport aircraft; definition of physical drag components

D Destarac, JJA Van Der Vooren - Aerospace science and technology, 2004 - Elsevier
Drag/thrust analysis of jet-propelled transonic transport aircraft on the basis of calculated
viscous flow is discussed. Unique definitions for viscous drag plus wave drag and for …

[HTML][HTML] Advancements and prospects of boundary layer ingestion propulsion concepts

NGM Moirou, DS Sanders, P Laskaridis - Progress in Aerospace Sciences, 2023 - Elsevier
The aviation sector is experiencing an increasing pressure to reduce emissions via long-
term strategies for a ceaselessly growing number of flight passengers. Aircraft currently in …

Coupling of turbulence wall models and immersed boundaries on Cartesian grids

SG Cai, J Degrigny, JF Boussuge, P Sagaut - Journal of Computational …, 2021 - Elsevier
An improved coupling of immersed boundary method and turbulence wall models on
Cartesian grids is proposed, for producing smooth wall surface pressure and skin friction at …

Exergy-based formulation for aircraft aeropropulsive performance assessment: theoretical development

A Arntz, O Atinault, A Merlen - AIAA journal, 2015 - arc.aiaa.org
Aircraft have evolved into extremely complex systems that require adapted methodologies
and tools for an efficient design process. A theoretical formulation based on exergy …

Full-aircraft energy-based force decomposition applied to boundary-layer ingestion

DS Sanders, P Laskaridis - AIAA Journal, 2020 - arc.aiaa.org
This Paper introduces a generic force decomposition method derived from mechanical
energy conservation. A transformation from relative to absolute reference frame captures the …

Performance bookkeeping for aircraft configurations with fuselage wake-filling propulsion integration

AL Habermann, J Bijewitz, A Seitz… - CEAS Aeronautical Journal, 2020 - Springer
The aim of this research is the identification of a unified bookkeeping and evaluation
scheme for the integrated performance analysis of a boundary layer ingesting (BLI) concept …

Numerical evaluation of entropy generation in isolated airfoils and Wells turbines

T Ghisu, F Cambuli, P Puddu, N Mandas, P Seshadri… - Meccanica, 2018 - Springer
In recent years, a number of authors have studied entropy generation in Wells turbines. This
is potentially a very interesting topic, as it can provide important insights into the …

[HTML][HTML] Pressure distribution guided supercritical wing optimization

LI Runze, D Kaiwen, Y Zhang, C Haixin - Chinese Journal of Aeronautics, 2018 - Elsevier
Pressure distribution is important information for engineers during an aerodynamic design
process. Pressure Distribution Oriented (PDO) optimization design has been proposed to …