27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-4.5.1

CRUISE NOX EMISSION REDUCTION BY THE RATIONAL CHOICE OF SUPERSONIC BUSINESS JET ENGINE DESIGN VARIABLES

A. A. Mirzoyan
CIAM, Russian Federation

Keywords: optimization, design variables, mission performance, engine, emission

The evaluation of the potentialities for maximal NOx emission reduction under specified noise, range and takeoff requirements was carried out in the work. Additional NOx emission reduction was indirectly provided by using low noise takeoff thrust management.

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