Results 11 to 20 of about 92,283 (210)

Manipulation of Leading-Edge Vortex Flow [PDF]

open access: yesAerospace, 2020
At very high angles of attack, the leading-edge vortex of a semi-slender delta wing becomes unsteady and collapses, endangering the flight stability. Active flow control by pulsed blowing stabilizes the vortex system, enlarging the flight envelope for such wing configurations.
Andrei Buzica, Christian Breitsamter
openaire   +3 more sources

Numerical Study on Vortical Flow Structure and Performance Enhancement of Centrifugal Compressor Impeller

open access: yesApplied Sciences, 2022
The performance and efficiency of a centrifugal compressor are usually affected by the highly complex 3-dimensional flow structures which develop in the flow field of the compressor.
Seongbin Hong   +2 more
doaj   +1 more source

Pulsed Blowing Interacting with a Leading-Edge Vortex

open access: yesAerospace, 2020
Manipulation of vortex instabilities for aerodynamic performance increase is of great interest in numerous aeronautical applications. With increasing angle of attack, the leading-edge vortex of a semi-slender delta wing becomes unsteady and eventually ...
Andrei Buzica, Christian Breitsamter
doaj   +1 more source

A Rotary Wing System for Micro Air Vehicle Applications. Part 1 [PDF]

open access: yesINCAS Bulletin, 2011
The goal of the paper is to propose a new type of ornithopter that avoids the mechanical difficulties of a flapping system. It uses a modified design of a cycloidal propulsor.
Valentin BUTOESCU
doaj   +1 more source

The Leading-Edge Structure Based on Geometric Bionics Affects the Transient Cavitating Flow and Vortex Evolution of Hydrofoils

open access: yesFrontiers in Energy Research, 2022
A hydrofoil is a fundamental structure in fluid machinery, and it is widely applied to the fields of propellers, blades of axial flow pumps and underwater machinery.
Hao Yan   +4 more
doaj   +1 more source

Numerical Investigation of a Dynamic Stall on a Single Rotating Blade

open access: yesAerospace, 2021
Dynamic stall is a phenomenon on the retreating blade of a helicopter which can lead to excessive control loads. In order to understand dynamic stall and fill the gap between the investigations on pitching wings and full helicopter rotor blades, a ...
Yin Ruan, Manfred Hajek
doaj   +1 more source

Effect of leading-edge tubercles on the flow over low-aspect-ratio wings at low Reynolds number

open access: yesTheoretical and Applied Mechanics Letters, 2023
Two-dimensional time-resolved particle image velocimetry (TR-PIV) and stereographic particle image velocimetry (SPIV) techniques were used to investigate the effect of leading-edge tubercles on the flow over low-aspect-ratio wing models.
Pengxin Yang, Yichen Zhu, Jinjun Wang
doaj   +1 more source

Numerical Studies on the Effect of Leading Edge Tubercles on a Low-Pressure Turbine Cascade

open access: yesEnergies, 2023
The influence of the bionic leading edge tubercles on the aerodynamic performance of a high-speed low-pressure turbine has been numerically studied. Nine different tubercle configurations were designed to reduce the loss of the cascade at high Mach and ...
Wenhua Duan   +3 more
doaj   +1 more source

Leading-edge vortex dynamics on plunging airfoils and wings [PDF]

open access: yesJournal of Fluid Mechanics, 2022
The vortex dynamics of leading-edge vortices on plunging high-aspect-ratio (AR = 10) wings and airfoils were investigated by means of volumetric velocity measurements, numerical simulations and stability analysis to understand the deformation of the leading-edge vortex filament and spanwise instabilities.
O. Son   +5 more
openaire   +4 more sources

Leading-Edge Vortex Lift (LEVL) Sample Probe for Venusian Atmosphere

open access: yesAerospace, 2022
Can a small, lightweight, free-falling sample probe be slowed enough in the Venusian atmosphere to run a 10 min microelectromechanical systems (MEMS) ion gas micro spectrometer, without adding a propulsion systems or explosives and parachutes to the ...
Christopher Isaac, Nick Jones
doaj   +1 more source

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