A Piper Cub aircraft configuration has been analyzed using the VSAERO code and the aerodynamic characteristics have been obtained at two incidences. Detailed pressure distributions have been computed along wing-body-tail sections. A comparison of lift characteristics with flight data shows reasonable agreement.
VSAERO Analysis of a Piper Cub Aircraft
1993
6 pages
Report
No indication
English
Aircraft , Aerodynamics , Aerodynamic characteristics , Body-wing and tail configurations , Computerized simulation , Piper aircraft , Computer programs , Panel method (Fluid dynamics) , Pressure distribution , Computational fluid dynamics , Two dimensional boundary layer , Viscous flow , Foreign technology
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