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Low speed aerodynamic test of large CROR aircraft model in a closed test section (L-CROR CTS)
Start date: Jun 25, 2012, End date: Dec 24, 2012 PROJECT  FINISHED 

"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."
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