Hot Annular Nozzle Cascade (HANC)


  • Closed-loop turbine nozzle flows
  • Aero and thermal performance testing
  • Main gas temperature up to 645 K (700°F, 380°C), 30 lbm/sec (14 kg/sec)
  • 280 K cooling air for secondary flows, individually metered and controlled
  • Diameters up to 1 m
  • Inlet pressure 3 psig
  • Ambient exit pressure