| 1. | Aérodynamique des hélicoptères et convertibles - publications - ONERA / DAAP |
| | A. Le Pape, J. Gatard, J.-C. Monnier, Experimental investigations of rotor-fuselage aerodynamic interactions using a helicopter powered model.... |
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| 2. | Turbine Test Bench VEGA2 - ONERA / DAFE-EN |
| | Since the realization of such a project is long and difficult, it was decided to define an intermediate first step that consists of building a more modest set up to study the aerodynamic interactions in transonic HP turbine.... |
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| 3. | Aerodynamics of Helicopters - Experimental Activities - ONERA / DAAP-EN |
| | Complete models of helicopters are used in the F1 wind tunnel in Le Fauga to study aerodynamic interactions.... |
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| 4. | Aerodynamics of Helicopters - Tilt-Rotor Aircraft - ONERA / DAAP-EN |
| | In this context, tests were performed in the LABM research wind tunnel in order to simulate the diverse aerodynamic interactions that occur on a tilt-rotor aircraft.... |
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| 5. | Aerodynamics of Helicopters - Publications - ONERA / DAAP-EN |
| | A. Le Pape, J. Gatard, J.-C. Monnier, Experimental investigations of rotor-fuselage aerodynamic interactions using a helicopter powered model.... |
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| 6. | Helicopters (HELI1) |
| | The presence of the rotor and its wake substantially modifies the flow on the helicopter fuselage.These aerodynamic interactions can have a decisive effect on flight qualities, performance, noise and vibrations.. Numerical computations are used to gain a better understanding of these interactions and optimise certain factors to improve the flight conditions.. |
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| 7. | RHILP [ Project Overview ] |
| | The prime objective of the RHILP project is to study some of the critical aspects of the Tilt-Rotor in order to reduce the development risk of a flying demonstrator : - Handling Qualities Criteria - Aerodynamic Interactions - Structural Transient Loads... |
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| 8. | WP3 [ ACT-TILT ] |
| | The coexistence of huge " proprotors " used over a large range of operating points (from a high thrust / horizontal disk position in hover to a much lower thrust vertical disk position in a 300Kts cruise) with a fixed-wing airframe results in a number of aerodynamic interactions unknown on more conventional aircraft.... |
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| 9. | RHILP [ tbd ] |
| | They mainly concern the aerodynamic interactions between rotors and wing, in helicopter mode, in hover and low speed conditions (nacelle angle between 80 ° and 100 ° and forward speeds up to 90 kts).... |
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