26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-1.2.2

DESIGN AND AERODYNAMIC ANALYSIS OF A LIGHT TWIN ENGINE PROPELLER AIRCRAFT

L. Pascale, F. Nicolosi*
Tecnam Aircraft Industries, Italy; *Second Univ. of Naples, Italy

Keywords: Aircraft Design, Light Twin-engine, Aerodynamic Analysis, Wind-Tunnel Tests

Design of a new twin propeller 4-seats light aircraft named P2006 has been carried out at Technam industries. The paper deals with aircraft design criteria and choice of the configuration. Results of a detailed numerical and experimental (wind-tunnel) aerodynamic analysis of P2006 performed at (DIAS-Univ. of Naples) are also presented.

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