• Acoustic measurements with the aim of improving jet flap interaction noise prediction
  • Wing surface unsteady pressure measurement to characterise the jet-flap interaction (JFI) and forward propagation
  • Acoustic directivity measurement at the tunnel wall for both the isolated and installed nacelle
  • Experimental and computational comparisons of noise prediction at take-off, landing, diversion and cruise conditions
  • Validation of wall-modelled LES for rapid low-frequency aeroacoustics simulation