Abstract
A numerical model for the viscous-inviscid interactive
computations ofrotor flows is presented. The basic methodology for
deriving the outer inviscid solution is a fully three-dimensional
boundary element method.The inner viscous domain, i.e. the
boundary layer, is described by the two-dimensional Navier-Stokes
equations
Original language | English |
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Title of host publication | Aerodynamics and Aeroacustics of Rotorcraf |
Place of Publication | Paris |
Publisher | AGARD |
Publication date | 1994 |
Publication status | Published - 1994 |
Event | Aerodynamics and Aeroacustics of Rotorcraf - Berlin Duration: 1 Jan 1994 → … |
Conference
Conference | Aerodynamics and Aeroacustics of Rotorcraf |
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City | Berlin |
Period | 01/01/1994 → … |