Published September 18, 2013
| Version v1
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A New Vertical Tail Design Procedure for General Aviation and Turboprop Aircraft
Description
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.
Notes
http://EWADE.AircraftDesign.org --- http://ProceedingsEWADE2013.AircraftDesign.org
Files
EWADE2013_Nicolosi.pdf
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(3.2 MB)
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