1,721,050 research outputs found

    Wind Tunnel Tests of the VG2-16 Airfoil

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    XII Congresso Nazionale AIDA

    Prediction of aerodynamic performance of airfoils in low Reynolds number flows

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    Presents a viscous/inviscid interaction procedure for the solution of incompressible flowfields with large laminar separated regions. The method extends previous work on prediction of aerofoil performance up to stall conditions. Shows how the existence of laminar separation bubbles is treated, and indicates how transition may be considered. Compares calculated results using this approach (MULTIM code) with experimental data for two common aerofoils at low Reynolds number. (from authors' abstract

    Aircraft Design through Numerical and Experimental Techniques Developed at DPA

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    Presented at Fourth European Workshop on Aircraft Design Education, Politecnico di Torino, 8-9 Maggio 200

    Design of a Three Surfaces R/C Aircraft Model

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    Presented at 2nd Advanced Engineering Design Conference, Glasgow, June 200

    Aircraft Design through Numerical and Experimental Techniques Developed at DPA

    No full text
    Presented at Fourth European Workshop on Aircraft Design Education, Politecnico di Torino, 8-9 Maggio 200
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