27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-4.8.1
PERFORMANCE SIMULATION OF AN IDEAL MIXER-EJECTOR TURBOFAN ENGINE FOR A SUPERSONIC BUSINESS JET
E. R. Rademaker
NLR, Netherlands
Keywords: turbofan, mixer-ejector, supersonic business jet
The NLR Gas Turbine Simulation Program GSP is used to carry out performance simulations for a noise reducing mixer-ejector engine variant for a supersonic business jet. The GSP mixer component has been modified to include the supersonic core flow. The paper shows the used method and results.
view full paper