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Design and Manufacturing of Baseline Low-Speed, Low-Sweep Wind Tunnel Model (EULOSAM)
Date du début: 1 juin 2013, Date de fin: 31 déc. 2016,
The EULOSAM project will deliver a large scale half-model to be tested in a pressurized low speed wind tunnel (WT). The model design will be performed under a previous CfP topic (JTI-CS-2010-3-SFWA-02-007), while Dassault Aviation will deliver a fuselage that has to be modified in order to fit the new laminar wing. The fuselage modifications must be designed in such a way that the fuselage can re ...
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