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 | 75th Fluid Dynamics Symposium: Aerodynamics and Aeroacoustics of Rotorcraft - Berlin, Germany Duration: 10 Oct 1994 → 13 Oct 1994 |
Conference
Conference | 75th Fluid Dynamics Symposium |
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Country/Territory | Germany |
City | Berlin |
Period | 10/10/1994 → 13/10/1994 |