(JTI-CS2-2016-CFP03-LPA-01-17) - WINDTUNNEL TEST FOR FLOW CONTROL AT THE ENGINE/PYLON WITH A REPRESENTATIVE AIRCRAFT CONFIGURATION UNDER FULLY REALISTIC FLOW CONDITIONS
Programme: Horizon 2020 Framework Programme
Call: Clean Sky 2 Call for Proposals 03 EU
Call: Clean Sky 2 Call for Proposals 03 EU
Topic description
Specific Challenge:
| To properly demonstrate the effect of flow control at the engine/pylon wind tunnel tests using a realistic detailed 3D model configuration under fully realistic flow conditions in terms of Mach number and Reynolds number are crucial. The model configuration will comprise a classic and an UltraHighBypass Ratio (UHBR) Turbofan nacelle with a cut back of the slats in the region of the pylon/wing, enabling a later translation of the flight test results with classic engines to the UHBR configuration. The wind tunnel tests shall be done with and w/o flow control, using pulsed jets, synthetic jets and steady blowing For the full topic description see the Call Text Document (Annex of Workplan) published with this call. |