| Nome |
# |
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Centre-Manifold Reduction of Bifurcating Flows, file e0c31c0c-9344-4599-e053-1705fe0aef77
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335
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Smart Morphing and Sensing for Aeronautical Configurations Prototypes, Experimental and Numerical : Findings from the H2020 N° 723402 SMS EU Project, file a503c133-6268-44cd-97a5-32d5b3d37130
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319
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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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256
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Experimental investigation of a helicopter rotor with Gurney flaps, file e0c31c0a-a6a4-4599-e053-1705fe0aef77
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253
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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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Secondary Instabilities of the In-Phase Synchronized Wakes Past Two Circular Cylinders in Side-By-side Arrangement, file e0c31c0c-9342-4599-e053-1705fe0aef77
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202
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On the Origin of the Flip-Flop Instability of two Side-by-Side Cylinder Wakes, file e0c31c0d-d410-4599-e053-1705fe0aef77
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173
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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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Efficient stabilization and acceleration of numerical simulation of fluid flows by residual recombination, file e0c31c0d-a2b3-4599-e053-1705fe0aef77
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124
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Implementation of [Gamma]-Re0 Transition Model within SU2: Model Validation and Verification, file 7867fb88-c6c0-4d8c-af8d-ff908ea821fc
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113
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Non-modal analysis of coaxial jets, file e0c31c0d-b991-4599-e053-1705fe0aef77
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113
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Computation of the bluff-body sound generation by a self-consistent mean flow formulation, file e0c31c0d-2e69-4599-e053-1705fe0aef77
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112
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MONNALISA: Modelling Nonlinear Aerodynamics of Lifting Surfaces, file ef2a2f65-3271-4154-b4b5-f95e100d3233
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96
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Linear stability of the steady flow past rectangular cylinders, file e0c31c12-33ed-4599-e053-1705fe0aef77
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92
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On the frequency selection mechanism of the low-Re flow around rectangular cylinders, file e0c31c12-bbbf-4599-e053-1705fe0aef77
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80
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Pressure from Tomographic PIV: the Schur Complement method, file e0c31c0f-257e-4599-e053-1705fe0aef77
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73
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An Almost Subharmonic Instability in the Flow Past Rectangular Cylinders, file 01cd31b5-11e9-4cc4-a89c-32143f9eafc7
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70
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First Instability and Structural Sensitivity of the Flow Past Two Side-by-Side Cylinders, file e0c31c0d-d753-4599-e053-1705fe0aef77
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70
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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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Global Stability and Sensitivity Analysis of Boundary-Layer Flows Past a Hemispherical Roughness Element, file e0c31c0d-d8e8-4599-e053-1705fe0aef77
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58
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Boundary-layer Flows Past an Hemispherical Roughness Element: DNS, Global Stability and Sensitivity Analysis, file e0c31c08-b618-4599-e053-1705fe0aef77
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55
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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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44
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An optimal, fast, parallel solver for the incompressible Navier-Stokes equations on colocated grids, file e0c31c11-c261-4599-e053-1705fe0aef77
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42
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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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Linear global stability of two incompressible coaxial jets, file e0c31c0d-d5c3-4599-e053-1705fe0aef77
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41
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A direction-splitting Navier–Stokes solver on co-located grids, file e0c31c11-ca9d-4599-e053-1705fe0aef77
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41
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On the Instability of the Flow Around Rectangular Cylinders, file e0c31c11-bcc5-4599-e053-1705fe0aef77
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38
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Global Stability and Sensitivity Analysis of Boundary-Layer Flows Past a Hemispherical Roughness Element, file e0c31c08-7397-4599-e053-1705fe0aef77
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35
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An almost subharmonic instability in the flow past rectangular cylinders, file 9278e5ab-80f7-4a87-99b4-960f84aa8876
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17
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An Almost Subharmonic Instability in the Flow Past Rectangular Cylinders, file 640dc72f-1573-449d-a022-2b8a8443b8fa
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11
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Aerodynamic Evaluation, file 7b16dc1a-3cab-4081-a304-226be6092cee
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11
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Linear global and asymptotic stability analysis of the flow past rectangular cylinders moving along a wall, file 904f379a-640d-4f3a-8244-6760938c1ea9
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10
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On the Origin of the Flip-Flop Instability of two Side-by-Side Cylinder Wakes, file e0c31c08-1cc9-4599-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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On the Origin of the Flip-Flop Instability of two Side-by-Side Cylinder Wakes, file e0c31c08-1cc8-4599-e053-1705fe0aef77
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3
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Computation of the bluff-body sound generation by a self-consistent mean flow formulation, file e0c31c0c-03d4-4599-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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An almost subharmonic instability in the flow past rectangular cylinders, file cdbfbd6a-d9ca-4f8c-ba3d-916cf72a56ba
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2
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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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Galerkin-Laguerre Spectral Solution of Self-Similar Boundary Layer Problems, file e0c31c07-f76d-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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First Instability and Structural Sensitivity of the Flow Past Two Side-by-Side Cylinders, file e0c31c08-21b1-4599-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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Boundary-layer Flows Past an Hemispherical Roughness Element: DNS, Global Stability and Sensitivity Analysis, file e0c31c08-9bd5-4599-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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A massively parallel, direction-splitting solver for DNS in complex geometries, file e0c31c0e-68eb-4599-e053-1705fe0aef77
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2
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Breathability of face mask materials in relation to the presence of melt blown fibers, file e0c31c11-201e-4599-e053-1705fe0aef77
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2
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A new scaling for the flow instability past symmetric bluff bodies, file e0c31c12-7ce7-4599-e053-1705fe0aef77
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2
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Bayesian calibration of a low order aerodynamic model for the design of unconventional tail empennages, file 6c7f5d9a-7af6-4bb5-8edb-d3f8f5fc0329
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1
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Numerical Investigation on the Stability of Singular Driven Cavity Flow, file e0c31c07-ce16-4599-e053-1705fe0aef77
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1
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Spectral Elliptic Solvers in a Finite Cylinder, file e0c31c07-d968-4599-e053-1705fe0aef77
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1
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Spectral Matrix Conditioning in Cylindrical and Spherical Elliptic Equations, file e0c31c07-deae-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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Efficient stabilization and acceleration of numerical simulation of fluid flows by residual recombination, file e0c31c0b-041f-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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Secondary Instabilities of the In-Phase Synchronized Wakes Past Two Circular Cylinders in Side-By-side Arrangement, file e0c31c0c-9343-4599-e053-1705fe0aef77
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1
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Scaling Laws for an Airfoil with MFC-Actuated Trailing Edge Plate, file e0c31c10-c446-4599-e053-1705fe0aef77
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1
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A direction-splitting Navier–Stokes solver on co-located grids, file e0c31c11-ca9e-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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Optimal initial perturbations in a boundary layer with wall actuation, file eedbe02a-35b4-4d31-a6a3-e574e7742fe3
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1
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| Totale |
3.405 |