Evaluation of low fidelity and CFD methods for the aerodynamic performance of a small propeller

EV Loureiro, NL Oliveira, PH Hallak… - Aerospace Science and …, 2021 - Elsevier
The increasing use of unmanned aerial vehicles and micro air vehicles creates a strong
demand for the accurate aerodynamic performance of small-diameters fixed-pitch …

Experimental Analysis of a Small‐Scale Rotor at Various Inflow Angles

A Kolaei, D Barcelos… - International Journal of …, 2018 - Wiley Online Library
The performance characteristics of a rotor that is typically used for small unmanned aircraft
were analyzed in a series of wind‐tunnel experiments. Wind‐tunnel measurements were …

A study on the efficient numerical analysis for the prediction of full-scale propeller performance using CFD

KW Kim, KJ Paik, JH Lee, SS Song, M Atlar… - Ocean …, 2021 - Elsevier
Abstract In Computational Fluid Dynamics (CFD) simulations, limited full-scale studies with
ship propellers have been conducted due to the limitation of computational resources and …

High altitude propeller design and analysis

J Morgado, M Abdollahzadeh, MAR Silvestre… - Aerospace Science and …, 2015 - Elsevier
This paper presents the design and optimization of a new propeller to use on the MAAT
cruiser airship. The inverse design methodology is based on minimum induced losses and …

Design and Performance Evaluation of Propeller for Solar‐Powered High‐Altitude Long‐Endurance Unmanned Aerial Vehicle

D Park, Y Lee, T Cho, C Kim - International Journal of …, 2018 - Wiley Online Library
Design, wind tunnel test, computational fluid dynamics (CFD) analysis, and flight test data
analysis are conducted for the propeller of EAV‐3, which is a solar‐powered high‐altitude …

Wind tunnel performance tests of the propellers with different pitch for the electric propulsion system

Z Czyż, P Karpiński, K Skiba, M Wendeker - Sensors, 2021 - mdpi.com
The geometry of a propeller is closely related to its aerodynamic performance. One of the
geometric parameters of a propeller is pitch. This parameter determines the distance by …

Aerodynamic optimization of propellers for high altitude pseudo-satellites

A García-Gutiérrez, J Gonzalo, D Domínguez… - Aerospace Science and …, 2020 - Elsevier
The propulsion system of High-Altitude Platform Stations or High-Altitude Pseudo-Satellites
(HAPS) is commonly based on propellers. The properties of the atmosphere at those high …

The reduction of quadcopter propeller noise

TA Brungart, ST Olson, BL Kline… - Noise Control …, 2019 - ingentaconnect.com
Fan affinity laws are combined with a simple scaling relationship for fan noise to show that
truly significant reductions in propeller noise can be achieved by increasing the propeller …

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 …

Characterizing and modeling the enhancement of lift and payload capacity resulting from thrust augmentation in a propeller-assisted flap** wing air vehicle

AE Holness, HA Bruck… - International Journal of …, 2018 - journals.sagepub.com
Biologically-inspired flap** wing flight is attractive at low Reynolds numbers and at high
angles of attack, where fixed wing flight performance declines precipitously. While the merits …