Abstract
This paper describes a new aerodynamic model for the flow past a complete helicopter in a generic flight state, with particular reference to hover and forward flight in ground effect. The model is based on an unsteady Reynoldsaveraged Navier-Stokes code,
| Original language | English |
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| Title of host publication | New Computational Models for Airframe Aerodynamics In- and Out of Ground Effect |
| Publication status | Published - 2010 |
| Event | CEAS, European Air and Space Conference - Duration: 1 Oct 2009 → … |
Conference
| Conference | CEAS, European Air and Space Conference |
|---|---|
| Period | 1/10/09 → … |