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Optimal High-Lift Turbine Blade Aero-Mechanical Design (ITURB)

Date du début: 1 oct. 2012, Date de fin: 30 juin 2015,

"The need for high speed low pressure turbine modules to be used with innovative aircraft engine concept establishes critical mechanical constraints with very high hub stresses for the rotor blades, thus representing a real challenge for the design. In order to assist the designer with reliable tools it is mandatory to assess the performance of turbine rotor blades of innovative concept with both ...
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