| Nome |
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Aerodynamic Interaction Between Rotor and Tilting Wing in Hovering Flight Condition, file e0c31c0d-9d7d-4599-e053-1705fe0aef77
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310
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Aerodynamic Shape Optimisation of a Proprotor and Its Validation by Means of CFD and Experiments, file e0c31c0c-5e89-4599-e053-1705fe0aef77
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302
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Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction, file e0c31c09-d77b-4599-e053-1705fe0aef77
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254
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Experimental investigation of a helicopter rotor with Gurney flaps, file e0c31c0a-a6a4-4599-e053-1705fe0aef77
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252
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Helicopter drag reduction by vortex generators, file e0c31c0c-28f0-4599-e053-1705fe0aef77
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213
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Proprotor–wing aerodynamic interaction in the first stages of conversion from helicopter to aeroplane mode, file e0c31c09-db06-4599-e053-1705fe0aef77
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207
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Simulation and Testing of Helicopter-Ship Aerodynamic Interaction, file e0c31c11-93c5-4599-e053-1705fe0aef77
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192
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Aerodynamic Blade Design with Multi-Objective Optimization for a Tiltrotor Aircraft, file e0c31c0d-c905-4599-e053-1705fe0aef77
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191
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Experimental Investigation of the Rotor-Wing Aerodynamic Interaction in a Tiltwing Aircraft in Hover, file e0c31c08-5e3d-4599-e053-1705fe0aef77
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178
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Analysis of the loads acting on the rotor of a helicopter model close to an obstacle in moderate windy conditions, file e0c31c0c-830a-4599-e053-1705fe0aef77
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170
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Wind-tunnel tests of the ERICA tiltrotor optimised air-intake, file e0c31c0d-efa3-4599-e053-1705fe0aef77
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150
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Assessment of 2D/3D Numerical Modeling for Deep Dynamic Stall Experiments, file e0c31c0d-c0ac-4599-e053-1705fe0aef77
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132
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Wind Tunnel Test of Drafting at Endurance Run Velocity, file e0c31c12-74ce-4599-e053-1705fe0aef77
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113
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Experimental Investigation on the Aerodynamic Interaction Between a Helicopter and Ground Obstacles, file e0c31c08-5e0f-4599-e053-1705fe0aef77
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107
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Dynamic Stall Inducted by Blade Vortex Interaction in Helicopter Descending Flight, file e0c31c0e-bf5f-4599-e053-1705fe0aef77
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104
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Perpendicular blade–vortex-interaction over an oscillating airfoil in light dynamic stall, file e0c31c09-d745-4599-e053-1705fe0aef77
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100
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MONNALISA: Modelling Nonlinear Aerodynamics of Lifting Surfaces, file ef2a2f65-3271-4154-b4b5-f95e100d3233
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95
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Wind Tunnel Investigation of a Helicopter Model in Shipboard Operations, file e0c31c0e-a220-4599-e053-1705fe0aef77
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89
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Experimental study of a helicopter model in shipboard operations, file e0c31c11-3846-4599-e053-1705fe0aef77
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83
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Rotor / Rotor Aerodynamic Interactions – a GARTEUR Action Group, file 52009b8c-4d21-41cb-a872-57484c16024f
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81
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Numerical assessment of an L-shaped Gurney flap for load control, file e0c31c0d-d08c-4599-e053-1705fe0aef77
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69
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Experimenting Rotorcraft Flight in Complex Environmental Conditions Using the Wind Tunnel: Helicopter Ship Landing Case, file b24596a7-36b5-4f20-a41e-328ba435d157
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68
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Stochastic Simulation of Ship Airwake in Helicopter Shipboard Operation, file cce606d8-24e8-4d63-b31c-b3eb10761799
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66
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Experimental assessment of an active L-shaped tab for dynamic stall control, file e0c31c0c-c0e9-4599-e053-1705fe0aef77
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63
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Stereo Particle Image Velocimetry Measurements of Perpendicular Blade-Vortex Interaction over an Oscillating Airfoil, file e0c31c0d-d4bd-4599-e053-1705fe0aef77
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63
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Experimental and Numerical Study of Parallel Blade-Vortex Interaction, file 70cdac91-b07d-48f5-9c5d-5bae7948a20d
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60
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A novel approach for reconstructing pressure from PIV velocity measurements, file e0c31c0d-d939-4599-e053-1705fe0aef77
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60
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Helicopter Noise in Urban Flight, file e0c31c11-b0fe-4599-e053-1705fe0aef77
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57
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Towards a Wind Tunnel Testing Environment for Rotorcraft Operations Close to Obstacles, file e0c31c0d-57b3-4599-e053-1705fe0aef77
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52
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Oscillating Aerofoil and Perpendicular Vortex Interaction, file e0c31c0d-a73f-4599-e053-1705fe0aef77
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45
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Robustness and limits of vortex generator effectiveness in helicopter drag reduction, file e0c31c0d-c5d4-4599-e053-1705fe0aef77
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43
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Infrared Thermography Measurements over a Tail-Plane Model of a Large Passenger Aircraft, file 06b3710f-f6ec-446a-a7e0-31f1934e7ba7
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41
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Experimental Investigation of a Trailing Edge L-shaped Tab on a Pitching Airfoil in Deep Dynamic Stall Conditions, file e0c31c0d-d32b-4599-e053-1705fe0aef77
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38
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Evaluation of Acoustic Shielding Effects from a Generic GARTEUR Helicopter Configuration, file e0c31c11-9af1-4599-e053-1705fe0aef77
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34
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CFD Analysis of Helicopter Wakes in Ground Effect, file e0c31c0c-9487-4599-e053-1705fe0aef77
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32
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Parallel Blade-Vortex Interaction on Pitching Airfoil, file e0c31c11-6717-4599-e053-1705fe0aef77
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25
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Aerodynamic Evaluation, file 7b16dc1a-3cab-4081-a304-226be6092cee
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11
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Experimental Investigation of Helicopter Noise While Approaching an Elevated Helipad, file 5b9981fd-f26b-460f-9b3b-0c89d3d16d68
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8
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Multi-Fidelity Numerical Approach to Aeroacoustics of Tandem Propellers in eVTOL Airplane Mode, file 5c2615e0-22dc-4974-81fa-c2620ec7fdfe
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6
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Assessment of 2D/3D Numerical Modeling for Deep Dynamic Stall Experiments, file e0c31c08-1ea1-4599-e053-1705fe0aef77
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5
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Helicopter drag reduction by vortex generators, file e0c31c08-c533-4599-e053-1705fe0aef77
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4
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Wind-tunnel tests of the ERICA tiltrotor optimised air-intake, file e0c31c0c-25ca-4599-e053-1705fe0aef77
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4
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Still air resistance during walking and running, file 5ec36abe-67f0-4064-ab23-36de261eb34f
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3
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Oscillating Aerofoil and Perpendicular Vortex Interaction, file e0c31c08-0cc3-4599-e053-1705fe0aef77
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3
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Assessment of 2D/3D Numerical Modeling for Deep Dynamic Stall Experiments, file e0c31c08-1ea2-4599-e053-1705fe0aef77
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3
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Experimental Investigation on the Aerodynamic Interaction Between a Helicopter and Ground Obstacles, file e0c31c08-1ea3-4599-e053-1705fe0aef77
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3
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Aerodynamic Interaction Between Rotor and Tilting Wing in Hovering Flight Condition, file e0c31c09-dacf-4599-e053-1705fe0aef77
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3
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Aerodynamic Blade Design with Multi-Objective Optimization for a Tiltrotor Aircraft, file e0c31c0a-7891-4599-e053-1705fe0aef77
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3
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Numerical assessment of an L-shaped Gurney flap for load control, file e0c31c0a-f789-4599-e053-1705fe0aef77
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3
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Experimental evaluation of the aerodynamic performance of a large-scale high-lift morphing wing, file e0c31c12-e7b7-4599-e053-1705fe0aef77
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3
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Wind-Tunnel Tests of a Tilt-Rotor Aircraft, file e0c31c07-dead-4599-e053-1705fe0aef77
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2
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Wing-Rotor Interactions on a 1/4 - Scale Tiltrotor Half-Model, file e0c31c08-11f1-4599-e053-1705fe0aef77
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2
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Experimental Investigation of a Trailing Edge L-shaped Tab on a Pitching Airfoil in Deep Dynamic Stall Conditions, file e0c31c08-1596-4599-e053-1705fe0aef77
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2
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Stereo Particle Image Velocimetry Measurements of Perpendicular Blade-Vortex Interaction over an Oscillating Airfoil, file e0c31c08-1d2b-4599-e053-1705fe0aef77
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2
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Reconstructing Pressure from PIV Velocity Measurements: a Novel Approach, file e0c31c08-1d64-4599-e053-1705fe0aef77
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2
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A novel approach for reconstructing pressure from PIV velocity measurements, file e0c31c08-2781-4599-e053-1705fe0aef77
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2
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Aerodynamics and Biomechanical Optimization of the Jump Phase in Skiing, Through a Simulation-Based Predictive Model, file e0c31c08-3262-4599-e053-1705fe0aef77
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2
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Experimental Investigation of the Rotor-Wing Aerodynamic Interaction in a Tiltwing Aircraft in Hover, file e0c31c08-4ec4-4599-e053-1705fe0aef77
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2
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Experimental Investigation of the Dynamic Stall Phenomenon on a NACA 23012 Oscillating Airfoil, file e0c31c08-7d57-4599-e053-1705fe0aef77
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2
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Wing-Rotor Aerodynamic Interference on a Tiltwing Aircraft in the First Part of Conversion Manoeuvre, file e0c31c09-cd44-4599-e053-1705fe0aef77
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2
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Proprotor–wing aerodynamic interaction in the first stages of conversion from helicopter to aeroplane mode, file e0c31c09-dafe-4599-e053-1705fe0aef77
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2
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Robustness and limits of vortex generator effectiveness in helicopter drag reduction, file e0c31c09-e67a-4599-e053-1705fe0aef77
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2
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Experimental Investigation on a 1/4 Scaled Model of an High-Performance Tiltwing Aircraft in Hover, file e0c31c0a-cb29-4599-e053-1705fe0aef77
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2
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Experimental Investigation of Unsteady Inflow for a Helicopter Model in Shipboard Operations, file e0c31c10-f025-4599-e053-1705fe0aef77
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2
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Unsteady load assessment of a scaled-helicopter model in a ship airwake, file e0c31c12-be1c-4599-e053-1705fe0aef77
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2
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Unsteady load assessment of a scaled-helicopter model in a ship airwake, file e0c31c12-dd32-4599-e053-1705fe0aef77
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2
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Chapter 60. Effects of seat and handgrips adjustments on a Hand Bike vehicle. An ergonomic and aerodynamic study for a quantitative assessment of Paralympics athlete’s performance, file e0c31c08-04a4-4599-e053-1705fe0aef77
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1
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Experimental Evaluation of an L-Shaped Tab to be Used as an Active Gurney Flap for Dynamic Stall Control, file e0c31c08-11ed-4599-e053-1705fe0aef77
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1
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Experimental Investigation of Perpendicular Vortex Interaction over an Oscillating Airfoil in Dynamic Stall Conditions, file e0c31c08-11ef-4599-e053-1705fe0aef77
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1
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Experimental Investigation of Perpendicular Vortex Interaction by Stereo Particle Image Velocimetry, file e0c31c08-5441-4599-e053-1705fe0aef77
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1
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Numerical Investigation of Three-Dimensional Effects on Deep Dynamic Stall Experiments, file e0c31c08-5443-4599-e053-1705fe0aef77
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1
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A Test Rig to Assess the Effectiveness of Drag Reduction Devices on a Heavy-Class Helicopter, file e0c31c08-bb22-4599-e053-1705fe0aef77
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1
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Numerical Investigation of Perpendicular Blade-Vortex-interaction on a Pitching Airfoil in Light Dynamic Stall, file e0c31c09-94d5-4599-e053-1705fe0aef77
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1
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Experiments on the Helicopter-Obstacle Aerodynamic Interference in Absence of External Wind, file e0c31c09-cd46-4599-e053-1705fe0aef77
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1
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Perpendicular blade–vortex-interaction over an oscillating airfoil in light dynamic stall, file e0c31c09-ce95-4599-e053-1705fe0aef77
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1
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CFD Assessment of the Helicopter and Ground Obstacles Aerodynamic Interference, file e0c31c0a-7a42-4599-e053-1705fe0aef77
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1
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Helicopter-Obstacle Aerodynamic Interaction in Windy Conditions, file e0c31c0b-2725-4599-e053-1705fe0aef77
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1
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Experimental assessment of an active L-shaped tab for dynamic stall control, file e0c31c0b-9421-4599-e053-1705fe0aef77
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1
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Experimental investigation of a helicopter rotor with Gurney flaps, file e0c31c0b-ffa6-4599-e053-1705fe0aef77
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1
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Wind-tunnel tests of a heavy-class helicopter optimised for drag reduction, file e0c31c0c-2906-4599-e053-1705fe0aef77
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1
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Experimental evaluation of the aerodynamic performance of a large-scale high-lift morphing wing, file e0c31c12-eda0-4599-e053-1705fe0aef77
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1
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| Totale |
4.248 |