Designing high aspect ratio wings: A review of concepts and approaches

Y Ma, A Elham - Progress in Aerospace Sciences, 2024 - Elsevier
In response to escalating environmental concerns and stringent economic constraints, there
is an urgent need to develop aircraft technologies and configurations that substantially …

[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 …

Optimising subgrid-scale closures for spectral energy transfer in turbulent flows

M Nabavi, J Kim - Journal of Fluid Mechanics, 2024 - cambridge.org
Subgrid-scale (SGS) modelling is formulated using a local transport of spectral kinetic
energy estimated by a wavelet multiresolution analysis. Using a spectrally and spatially local …

[PDF][PDF] Propeller thrust explained by Newtonian physics.

MN Landell-Mills - Pre-Print DOI, 2021 - researchgate.net
Newtonian physics provides a straightforward explanation of the forces created by all
propellers, rotors and wings. The propeller passes through a mass of air each second (m/dt) …

Scale effect on wave planing performance of amphibious aircraft at constant speed

J Chen, L Li, X Fu, T Xiao, B Wu, M Tong - Aerospace Science and …, 2024 - Elsevier
Scaled model testing is commonly recognized as a valuable approach for predicting aircraft
performance in the aeronautical applications. However, challenges arise in the case of wave …

Cost effectiveness and feasibility considerations on the design of mini-UAVs for balloon takedown. Part 2: Aircraft design approach selection

L Piancastelli, C Leon-Cardenas, E Pezzuti… - Cogent …, 2023 - Taylor & Francis
The widespread availability of cheap, mass-produced balloons puts a strain on the financial
and manufacturing capacities of most aerial interception systems. In the past, high-altitude …

Numerical and experimental research on flight control of a V-Tail configuration for the wind tunnel model of aircraft

J Liu, W Qian, Y Bai, X Xu - Aerospace, 2022 - mdpi.com
The V-tail configuration has excellent stealth performance and has been using widely in the
aerodynamic shape design of advanced aircraft. Many recent studies have focused on …

Identification of Lateral-Directional Aerodynamic Parameters for Aircraft Based on a Wind Tunnel Virtual Flight Test

S Tai, L Wang, Y Wang, S Lu, C Bu, T Yue - Aerospace, 2023 - mdpi.com
In the early stages of aircraft design, a scaled model of the aircraft is installed in a wind
tunnel for dynamic semi-free flight to approximate real flight, and the test data are then used …

Recommendations on Increased Use of Modelling and Simulation for Certification/Qualification in Aerospace Industry

F Vetrano, P Worton, H Smaoui, A Szukala… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
The perspective of the Aerospace industry, both civil and military, is constantly evolving in
response to international crises, environmental footprint, sustainability expectations etc. The …

[PDF][PDF] Scaled flight testing for evaluating distributed electric propulsion

H Jentink, C Döll, P Iannelli, M Hoogreef… - Proc. 34th ICAS …, 2024 - pure.tudelft.nl
Abstract The potential of Distributed Electric Propulsion (DEP) for future aircraft has been
evaluated with Scaled Flight Testing (SFT). Scaled flight testing can contribute to a reduction …