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.

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