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title: 47th AIAA Aerospace Sciences Meeting including
The New Horizons Forum and Aerospace Exposition
`The Rakelet' - A Wingtip Modification Approach to Improve Endurance, Range and Fuel Savings
2-D Circulation Control Airfoil Benchmark Experiments Intended for CFD Code Validation
2-D Circulation Control Airfoil Benchmark Experiments Intended for CFD Code Validation
2-D Numerical Analysis of a VAWT Wind Farm for Different Configurations
2-D NUMERICAL ANALYSIS OF A VAWT WIND FARM FOR DIFFERENT CONFIGURATIONS
2D Plasma Flow in a Magnetic Nozzle with a Bi-Modal Electron Energy Distribution Function
2D Plasma Flow in a Magnetic Nozzle with a Bi-Modal Electron Energy Distribution Function
2-D Simulations of Single and Double DBD Plasma Actuators with Finite Electrode Thicknesses
3-D Adaptive Eulerian-Lagrangian Method for Gravity- and Capillarity-Induced Flows
3-D Adaptive Eulerian-Lagrangian Method for Gravity- and Capillarity-Induced Flows
3D Dynamic Stall Modelling on the NREL Phase VI Parked Blade
3D Dynamic Stall Modelling on the NREL Phase VI Parked Blade
3D Flapping Aerodynamic Comparisons Of Corrugated Wing Vs. Flat Plate
3D Flapping Wing Simulation with High Order Spectral Difference Method on Deformable Mesh
3D FLAPPING WING SIMULATION WITH HIGH ORDER SPECTRAL DIFFERENCE METHOD ON DEFORMABLE MESH
3-D Flight Plan for an Autonomous Aircraft
3-D FLIGHT PLAN FOR AN AUTONOMOUS AIRCRAFT
3-Dimensional Tree-Based Trajectory Planning with Highly Maneuverable Vehicles
3-DIMENSIONAL TREE-BASED TRAJECTORY PLANNING WITH HIGHLY MANEUVERABLE VEHICLES
3-D Multiscale Adaptive Eulerian-Lagrangian Method for Multiphase Flows with Phase Change
3-D MULTISCALE ADAPTIVE EULERIAN-LAGRANGIAN METHOD FOR MULTIPHASE FLOWS WITH PHASE CHANGE
3-D WAKE DYNAMICS OF THE VAWT: EXPERIMENTAL AND NUMERICAL INVESTIGATION
3-D Wake Dynamics of the VAWT: Experimental and Numerical Investigation
3rd Order Upwind Residual Distribution Schemes on Isoparametric Curved Elements
40 years with Swirl, Vortex, Cyclonic Flows, and Combustion
40 YEARS WITH SWIRL, VORTEX, CYCLONIC FLOWS, AND COMBUSTION
80% Scaled NASA Common Research Model Wind Tunnel Test of JAXA at Relatively Low Reynolds Number