| 1. | No title |
| | The first straightforward applications involved static modeling, such as ground effects or hinge moment identification from flight and wind tunnel tests.... |
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| 2. | RHILP [ News ] |
| | In WP2 the partners have analyzed the specific phenomena of a tilt-rotor (wing down-load, fountain flow effect, ground effect...). Simplified modelling of these phenomena has been developed for off-line and real time simulations.... |
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| 3. | RHILP [ Modelling WT Tests ] |
| | Tests for isolated rotor and half model with and without a symetry plane have been performed in hover and low forward speed in the helicopter mode for both in and out of ground effect.... |
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| 4. | odas2011 |
| | Numerical Simulation and Modelling of High-Lift Aerodynamics in Ground-Effect... |
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| 5. | RHILP [ tbd ] |
| | Influence of the ground effect on the download... Wing download evolution in ground effect is obtained by using published data from tests of small-scale Tiltrotor model.... |
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| 6. | RHILP [ tbd ] |
| | These test have been performed in Hover and in low speed Forward Flight " out of ground effect (OGE) " and " In ground effect (IGE) for 2 positions " and for wing flap setting between 0 ° and 80 °.... |
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| 7. | RHILP [ tbd ] |
| | The more interesting results concern the wing download.With nacelle angle set to 90 ° degrees (helicopter mode) following effects have been investigated at different wing flap settings and rotor thrust levels : - ground effect, - fountain flow effect, - rotor to wing distance, - lateral flapping of rotor disc.. |
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