Zobrazeno 1 - 10
of 187
pro vyhledávání: '"Clean Sky 2"'
Publikováno v:
Aerospace, Vol 9, Iss 4, p 204 (2022)
The authors have adjusted the DLR forecast model to evaluate the environmental benefits in terms of CO2 and NOx emissions of Clean Sky 2 technology innovations. The paper briefly describes the model employed: it consists of a passenger/flight volume
Externí odkaz:
https://doaj.org/article/ce92096ea84a415bbdbc6d48dc602681
Autor:
Simonassi, Loris, Lopes, Gustavo, Gendebien, Samuel, Torre, Antonino Federico Maria, Patinios, Marios, Lavagnoli, Sergio, Zeller, Nicolas, Pintat, Ludovic
Publikováno v:
Volume 10B: Turbomachinery — Axial Flow Turbine Aerodynamics; Deposition, Erosion, Fouling, and Icing; Radial Turbomachinery Aerodynamics
The ultra-high bypass ratio geared turbofan is a key concept to reduce the environmental impact of the next generation aircrafts. The increase in rotational speed of the low-pressure turbine (LPT) enabled by the geared architecture offers potential b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d62a050d3f50d6164f5dac1a0b39e8cf
https://zenodo.org/record/8174514
https://zenodo.org/record/8174514
Autor:
Torre, Antonino Federico Maria, Patinios, Marios, Lopes, Gustavo, Simonassi, Loris, Lavagnoli, Sergio
Publikováno v:
J. Turbomach.
In this article, a numerical investigation of the effect of a miniaturized five-hole probe downstream of a transonic low-pressure turbine vane row is presented. First, a numerical calibration of the probe was performed in uniform flow conditions, as
Publikováno v:
Aerospace, Vol 8, Iss 3, p 66 (2021)
The present work is part of the Clean Sky 2 project Full-Fairing Rotor Head Aerodynamic Design Optimization (FURADO), which deals with the aerodynamic design optimization of a full-fairing rotor head for the Rapid And Cost-Effective Rotorcraft (RACER
Externí odkaz:
https://doaj.org/article/b4310d303b4d453c894e6809bf8b2a33
Publikováno v:
Aerospace, Vol 8, Iss 2, p 52 (2021)
One of the crucial issues affecting the structural safety of propeller vehicles is the propeller tonal excitation and related vibrations. Propeller rotation during flight generates vibrating sources depending upon its rotational angular velocity, num
Externí odkaz:
https://doaj.org/article/bf8b3819b2c84d56bdcc0814edd20afa
Autor:
Dostal, Martin
The rapidly growing air traffic density and the introduction of new technology have dramatically increased flight safety in the last 30 years while significantly increasing the complexity of the flying tasks and the flight deck human-machine interfac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::22cf4ab06fd2607c42f7fccad4b813cc
The aerodynamics of a high-speed low-pressure turbine (LPT) cascade was investigated under steady and unsteady flow conditions. The tests were performed at outlet Mach (M) and Reynolds numbers (Re) of 0.90 and 70k, respectively. Unsteady wakes were s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1b01916986f28cf214c497fd3582ea5f
The influence of the unsteady wakes incoming from the upstream stages is of high relevance in modern high-speed low pressure turbines operating at transonic exit Mach numbers and low-Reynolds numbers, for their potential to trigger transition and inf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::50a4cae9eea7bc331e17d38ad825a88b
This project has received funding from the Clean Sky 2 Joint Undertaking (JU) under grant agreement No 945583. The JU receives support from the European Union’s Horizon 2020 research and innovation programme and the Clean Sky 2 JU members other tha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1842e8cc83e067c22bf46f14bad79367