Objective "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." Fields of science engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraft Programme(s) FP7-JTI - Specific Programme "Cooperation": Joint Technology Initiatives Topic(s) JTI-CS-2012-1-SFWA-02-028 - Low speed aerodynamic test of large CROR aircraft model in a closed test section Call for proposal SP1-JTI-CS-2012-01 See other projects for this call Funding Scheme JTI-CS - Joint Technology Initiatives - Clean Sky Coordinator STICHTING DUITS-NEDERLANDSE WINDTUNNELS EU contribution € 1 499 880,00 Address VOORSTERWEG 31 8316 PR Marknesse Netherlands See on map Region Oost-Nederland Flevoland Flevoland Activity type Research Organisations Administrative Contact Oliver Fries (Mr.) Links Contact the organisation Opens in new window Website Opens in new window Total cost No data
