outcomes

 
 

Main expected results/deliveries:

Design and structural testing of a fully integrated wing leading edge section featuring advanced HLFC technology [TS1]

  • Innovative WIPS for laminar wing
  • Krueger flap linkage system
  • Collapsible CFRP Krueger panel with folding bull nose
  • Assessment of ALT device

Engineering feasibility of advanced HLFC technology applied on fin proven by means of prototype demonstration in operational environment [TS1]

Progress so far on HYBRID LAMINAR FLOW CONTROL (TS1)


Experimental demonstration of locally applied active flow control technologies for performance increase and/or loads control [TS2, TS3]

Progress so far on ACTIVE FLOW CONTROL ON AIRFRAME (TS2, TS3)


Engineering feasibility of noise and vibrations mitigation technologies proven by means of prototype demonstration in operational environment [TS5, TS6]

  • Improve design and analysis from dynamic point of view (transient and aeroelastic response)
  • Improvement of landing gear doors manufacturing process (new materials, new design principles)
  • PFSE for airframe noise reduction

Progress so far on NOISE CONTROL ON AIRFRAME (TS5)

Progress so far on CONTROL MEANS FOR VIBRATION AND AEROELASTIC COUPLING (TS6)


Assessment of novel trailing edge flow control concepts [TS4]

Progress so far on MULTIFUNCTIONAL TRAILING EDGE CONCEPTS (TS4)