Drone (UAV) Online Courses
Here's every CFD online course related to Drone (UAV) category.
Quadcopter Fluid-Structure Interaction (FSI) Simulation using ANSYS Fluent
Intermediate, Advanced
Price: $649
This study presents a Fluid-Structure Interaction (FSI) simulation of a quadcopter using ANSYS Fluent The quadcopter geometry was created using ANSYS SpaceClaim The model was then meshed using ANSYS Meshing, which generated an unstructured mesh consisting of approximately 499,152 elements To accurately capture the blades’ rotation, two frame motion(MRF) zones are applied to the blades. The Structure model with the Linear Elasticity option was enabled to investigate the displacement of the blade
Javelin Rocket Motion Simulation with Dynamic Mesh Method (Six DOF) using ANSYS Fluent
Intermediate, Advanced
Price: $429
This report presents a simulation of the motion of a javelin rocket using the dynamic mesh method The geometry of the javelin rocket is created using Spaceclaim software A high-quality mesh is generated around the rocket geometry using ANSYS Meshing(about 250,000 elements) The six DOF solver settings are specified, including the mass properties and the degrees of freedom for translation and rotation.
Price: $649
The problem numerically simulates the Dynamic Stability Derivatives of the Javelin Rocket using ANSYS Fluent. We designed the 3-D model using the SpaceClaim. We mesh the model with ANSYS Meshing software, and the element number equals 4,245,614. We perform this simulation as unsteady (Transient). We use the Mesh Motion and UDF files to define the rotational and oscillation motion of the Rocket.
Price: $319
This problem simulates a javelin rocket using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using ANSYS Meshing. The simulation is carried out using the density-based solver. The turbulence model is set to Realizable k-ε.
FSI Analysis for Northrop Grumman RQ-4 Global Hawk, ANSYS Fluent
Intermediate, Advanced
Price: $489
The problem numerically simulates the Fluid-Structure Interaction over Northrop Grumman RQ-4 Global Hawk using ANSYS Fluent software. The Global Hawk geometry was modeled using SpaceClaim and then imported into ANSYS meshing for meshing consisting of 5,056,067 non-conformal elements. The simulation used a pressure-based solver. One way FSI model analyses total strain, and stress over the turbine.
Northrop Grumman RQ-4 Global Hawk Analysis CFD Simulation, ANSYS Fluent
Beginner, Intermediate
Price: $219
This study aims to investigate the aerodynamic performance of a Grumman RQ-4 Global Hawk using ANSYS Fluent. The Global Hawk geometry was modelled using SpaceClaim then imported into ANSYS Fluent for meshing consisting 3,764,695 elements. The simulation used a pressure-based solver.
Price: $649
In this study, a comprehensive acoustic simulation of a quadcopter was performed using ANSYS Fluent Studying Acoustic, Pressure, and Motion analysis. We designed the 3-D symmetry model using the SpaceClaim We mesh the model with ANSYS Meshing software, and the element number equals 1,710,236. We perform this simulation as unsteady (Transient). We use the Mesh Motion to define the rotational motion of the Quadcopter blades.
Price: $649
The problem numerically simulates the dynamic stability derivatives of a flying wing aircraft using ANSYS Fluent The Mesh Motion and UDF files are used to define the rotational and oscillatory motion of the wing. The 3D geometry of the model was created using ANSYS SpaceClaim A high-quality unstructured mesh was generated using ANSYS Meshing The corresponding graphs are drawn and the total number of 24 dynamic derivatives coefficients are correctly extracted.
RQ-170 UAV Simple Aerodynamic Analysis: CFD Simulation by ANSYS Fluent
Beginner, Intermediate
Price: $219
The problem numerically simulates an RQ-170 UAV using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software. The element number equals 2,415,175 and their type is polyhedra.