Aeroacoustic interactions of blade skew and leading edge serrations applied to low-pressure axial fans

TM Biedermann, N Hintzen… - … of Engineering for …, 2022 - asmedigitalcollection.asme.org
Leading edge serrations are well known for their ability to reduce turbulence-induced noise
of single airfoils while also providing aerodynamic advantages under certain operating …

Impact onto the boundary layer on the airfoil of a small-scale aircraft system with the use of a wavy surface. Problems and Prospects

ID Zverkov, AV Kryukov - Journal of Applied Mechanics and Technical …, 2021 - Springer
A method is proposed to improve the aerodynamic performance of small-scale aircraft
systems. The method is based on fundamental gas-dynamic phenomena, such as local …

Various Wavy Leading-Edge Protuberance on Oscillating Hydrofoil Power Performance

A Abbasi, H Ghassemi, H Ghafari… - Journal of Applied Fluid …, 2023 - jafmonline.net
This paper is presented to compare various wavy leading-edge protuberances on oscillating
hydrofoil performance and power efficiency. The unsteady turbulent 3D flow simulations …

[PDF][PDF] Воздействие на пограничный слой крыла малоразмерного летательного аппарата с помощью волнистой поверхности. Проблемы и перспективы …

ИД Зверков, АВ Крюков - Прикладная механика и техническая физика, 2021 - sibran.ru
Представлен способ улучшения аэродинамических характеристик малоразмерных
летательных аппаратов, основанный на таких фундаментальных газодинамических …

[PDF][PDF] COB-2023-0221 COMPUTATIONAL ANALYSIS OF THE EFFECT OF WAVY LEADING EDGE ON STABILIZER

P Gonzalez-DeGreiff, W Gomez-Rivera… - researchgate.net
Wavy Leading Edge (WLE) is a bio-mimetic device inspired by the tubercles found on
humpback whales. Generated by a sinusoidal function, they alter the flow field around the …

[PDF][PDF] IMPACT ONTO THE BOUNDARY LAYER ON THE AIRFOIL OF A SMALL-SIZED FLYING VEHICLE WITH THE USE OF A WAVY SURFACE. PROBLEMS AND …

AV Kryukov - researchgate.net
A method is proposed to improve the aerodynamic performance of small-sized flying
vehicles. The method is based on fundamental gas-dynamic phenomena, such as local …