• Experimental and numerical quantification of exhaust suppression effect at wind-milling due to aerodynamic interaction with the airframe wing
  • Independent control of core and fan nozzle pressure ratio
  • Generation of high quality experimental database for numerical validation
  • Demonstration of ARA Binary Pressure-Sensitive Paint (PSP) system
  • Validation of RANS CFD ability to predict wing-installed exhaust aerodynamic performance
  • Zero-Dimensional engine performance simulation to quantify impact of airframe-installed exhaust suppression on engine re-matching and ingested mass flow at wind-milling
Dual Stream Jet Propulsion Rig in the ARA Transonic Wind Tunnel

RANS CFD prediction of installed exhaust static pressure distribution at wind-milling
RANS CFD prediction of installed exhaust static pressure distribution at wind-milling
Dual Stream Jet Propulsion Rig installed in the ARA Transonic Wind Tunnel