Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Antonio Visingardi"'
Publikováno v:
Applied Sciences, Vol 11, Iss 20, p 9664 (2021)
The Italian research project PROSIB (PROpulsione e Sistemi IBridi per velivoli ad ala fissa e rotante), is a 30-month initiative funded by the Italian Ministry of University and Scientific Research (MIUR) and coordinated by the Leonardo company. The
Externí odkaz:
https://doaj.org/article/4789bf5d964f46e6a9196158ad8976ea
Publikováno v:
Energies, Vol 14, Iss 9, p 2613 (2021)
The rotor wake aerodynamic characterization is a fundamental aspect for the development and optimization of future rotary-wing aircraft. The paper is aimed at experimentally and numerically characterizing the blade tip vortices of a small-scale four-
Externí odkaz:
https://doaj.org/article/b238ba624cdb430e89a821eed2cf7382
Autor:
Salvatore Ameduri, Antonio Concilio, Antonio Visingardi, Luigi Federico, Mattia Barbarino, Pier Luigi Vitagliano
Publikováno v:
ASME 2022 Conference on Smart Materials, Adaptive Structures and Intelligent Systems.
In line with target of the European Project “Shape Adaptive Blades for Rotorcraft Efficiency-SABRE”, that is to say, to mitigate the environmental impact of the rotorcraft, a Shape Memory Alloy (SMA) morphing twist systems was developed and relat
Publikováno v:
Energies, Vol 14, Iss 2613, p 2613 (2021)
Energies; Volume 14; Issue 9; Pages: 2613
Energies; Volume 14; Issue 9; Pages: 2613
The rotor wake aerodynamic characterization is a fundamental aspect for the development and optimization of future rotary-wing aircraft. The paper is aimed at experimentally and numerically characterizing the blade tip vortices of a small-scale four-
Publikováno v:
Experiments in Fluids. 61
The aim of the article is to propose a simple engineering method for identifying and characterizing vortical structures within a flow field measured with a classic two-component PIV measurement system. Some of the most popular vortex detection system
Publikováno v:
AIAA Journal. 49:1614-1624
Publikováno v:
AIAA Journal. 45:751-759
The present paper illustrates a computational aeroacoustic method for evaluating the effects of airframe scattering on the noise generated by a tilt-rotor system under realistic operating conditions. The physical model assumes ideal fluid, irrotation
Publikováno v:
16th AIAA/CEAS Aeroacoustics Conference.
The problem of helicopter noise generation, fuselage scattering and propagation in an urban environment is solved using a CAA wave splitting technique based on a coupled FW-H/FEM computation. This original technique allows the forward and backward pr
Publikováno v:
12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference).