Speeding RTM with heat-flux sensors: Clean Sky 2 INNOTOOL 4.0 project advances cure monitoring for larger and less costly lightweight landing gear made using composites.

Autor: Gardiner, Ginger ginger@compositesworld.com

Publikováno v: CompositesWorld. Jul2021, Vol. 7 Issue 7, p30-35. 5p.

Recent developments of common numerical methods and common experimental means within the framework of the large passenger aircraft program

Autor: Boden, Fritz, Barth, Hans Peter, Hein, Stefan, Heitmann, Dirk, Kirmse, Tania, Klein, Christian, Krüger, Wolf-Reiner, Lemarechal, Jonathan, Norambuena, Marco, Schäfer, Dominik, Schnell, Rainer, Sinha, Kautuk, Theiß, Alexander, Weiss, Armin

Publikováno v: CEAS Aeronautical Journal. 14:281-293

For the exploration and validation of the integration of efficient propulsion concepts and new technologies for future large passenger aircraft, it is necessary to establish suitable design, evaluation and measurement tools. Therefore, as one major a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0c9aef940a82a8ed4dacddda700935c0
https://doi.org/10.1007/s13272-022-00635-w

Vane–Probe Interactions in Transonic Flows

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

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::61f7412f6349a05d7afe6a93e8bd79ca
https://doi.org/10.1115/1.4056578

An Experimental Test Case for Transonic Low-Pressure Turbines – Part I: Rig Design, Instrumentation and Experimental Methodology

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

Vibration Response Aspects of a Main Landing Gear Composite Door Designed for High-Speed Rotorcraft

Autor: Maurizio Arena, Antonio Chiariello, Martina Castaldo, Luigi Di Palma

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