Engineering method to estimate the blade loading of propellers in nonuniform flow

N van Arnhem, R de Vries, T Sinnige, R Vos… - AIAA Journal, 2020 - arc.aiaa.org
Advances in aerodynamic and propulsive efficiency of future aircraft can be achieved by
strategic installation of propellers near the airframe. This paper presents a robust and …

Aerodynamics and flight mechanics analysis of Airbus Helicopters' compound helicopter RACER in hover under crosswind conditions

J Thiemeier, C Öhrle, F Frey, M Keßler… - CEAS Aeronautical …, 2020 - Springer
In recent years, various helicopter manufacturers have been focusing increasingly on the
development of new high-speed rotorcraft configurations, one of them being the compound …

The effect of a flow field on chemical detection performance of quadrotor drone

S Do, M Lee, JS Kim - Sensors, 2020 - mdpi.com
The determination of a suitable sensor location on quadrotor drones is a very important
issue for chemical reconnaissance platforms because the magnitude and direction of air …

Analysis of quadcopter propeller vibration based on laser vibrometer

E Kuantama, OG Moldovan, I Ţarcă… - Journal of Low …, 2021 - journals.sagepub.com
An unbalanced propeller can affect a quadcopter's performance due to vibration, also
decreasing its thrust's yield. Analyses were conducted to determine the correlation between …

Aerodynamic impact of a streamwise vortex on a propeller

Y Yang, LLM Veldhuis, G Eitelberg - Aerospace Science and Technology, 2017 - Elsevier
In some situations, a vortex is involved in the inflow of a propeller, eg a ground vortex or a
vortex shed from the upstream parts of the airframe of the aircraft. In order to study the impact …

Vortex model and blade span influence on orthogonal blade-vortex interaction noise

P Zehner, F Falissard, X Gloerfelt - AIAA Journal, 2020 - arc.aiaa.org
The influence of the vortex impingement location on the aerodynamic and acoustic response
of a rotating blade during an orthogonal interaction is studied by means of computational …

Investigation on the dynamic response of a wide-chord fan blade under ground vortex ingestion

Z Wang, Y Chen, H Ouyang, A Wang - International Journal of …, 2019 - Springer
This paper presents a computational study of the dynamic response of the fan blade owing
to the excitations from the ingested ground vortex when the turbofan engine is operating on …

Propulsion Configuration Design and Analysis for an eVTOL Passenger Air Shuttle

N Ayar, M Ahmed, K Nocon, R Patel… - 2021 AIAA/IEEE …, 2021 - ieeexplore.ieee.org
This paper describes the design maturation of an electric vertical take-off and landing
(eVTOL) aircraft for urban air mobility. This work aims to build upon previous work on the …

Wind turbine wake vortex influence on safety of small rotorcraft

BG van der Wall - The Aeronautical Journal, 2019 - cambridge.org
The wake vortex of lifting surfaces such as wind turbine blades or fixed-wing aircraft can
heavily affect the blade aerodynamics of rotorcraft. Using blade element theory, the pilot …

[PDF][PDF] Advances in PIV Uncertainty Quantification Towards a Comprehensive Framework

S Adatrao - 2023 - pure.tudelft.nl
Summary Particle Image Velocimetry (PIV) is a leading technique that allows flow velocity
measurements in two-and three-dimensional domains. PIV is a fullfield, non-intrusive and …