Helicopter Rotor Airloads Prediction Using CFD and Flight Test Measurement in Hover Flight

Davoud Hassanzadeh

Volume 9, Issue 1 , March 2012

Abstract
  An implicit unsteady upwind solver including a mesh motion approach was applied to simulate a helicopter including body, main rotor and tail rotor in hover flight. The discretization was based on a second order finite volume approach with fluxes given by the Roeand#39;s scheme. Discretization of Geometric ...  Read More