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Low speed aerodynamic test of large CROR aircraft model in a closed test section (L-CROR CTS)
Date du début: 25 juin 2012, Date de fin: 24 déc. 2012 PROJET  TERMINÉ 

"Tests will be performed on a full model with installed CROR engines. The model will be mounted on a ventral sting, located at tunnel centre line. The model is provided with two powered Counter-Rotating propellers which are driven by two air motors (owned by the Topic Manager).The aim of the test is to determine the aerodynamic performance and stability & control characteristics of a CROR powered aircraft. During the test, innovative measuring techniques and hardware solutions will be used to assess the aerodynamic signature.The test will be performed in the 8mx6m closed test section of DNW-LLF."