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Intermediate Compressor Case Duct Aerodynamics - JTI-CS2-2017-CFP06-ENG-03-19
Date de clôture : 21 juin 2017  

 Technologie aérospatiale
 Industries aéronautiques

Specific Challenge:

An experimental test campaign is planned to be performed to verify that the design of the demonstrator ICC performs as predicted. In a second test campaign new technologies and innovative duct designs will be studied. The duct flowfield will be characterized in detail in order to provide validation data for CFD methods. Off-design performance will be of specific interest to this exercise. Development of CFD tools, including more advanced modelling techniques (such as hybrid LES methods) will be an important task to be able to predict part-speed performance and separation margin of the ICC duct. Please refer to the full and formal topic descriptions published in this call.

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