Published September 18, 2013 | Version v1
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A New Vertical Tail Design Procedure for General Aviation and Turboprop Aircraft

  • 1. University of Naples "Federico II"


A new procedure to evaluate the aerodynamic interference of airplane’s components on the vertical tailplane has been proposed. It has been developed by solving Navier-Stokes equations in a fully turbulent subsonic flow regime on more than 200 regional turboprop aircraft configurations, with the aim to bring CFD into aircraft preliminary design.

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