Compressible Flow Online Courses
Here's every CFD online course related to Compressible Flow category.
Price: $20
The present CFD Project simulates compressible air flow over Naca 0012 airfoil via ANSYS Fluent software. We modeled the geometry using ANSYS Design Modeler software and created the mesh using ANSYS Meshing software. The mesh type is structured, and the number of cells f is 1,560,000. The air property is selected as the ideal gas to model compressibility.
Supersonic Flow over SR-71 Blackbird CFD Simulation
Intermediate
Price: Free
The present CFD Project simulates supersonic airflow over SR-71 blackbird aircraft via ANSYS Fluent software. We modeled the geometry using ANSYS Design Modeler software and created the mesh using ANSYS Meshing software. The meshing is Polyhedra, and the number of cells is 1,744,624. the air property is selected as the ideal gas to model compressibility.
Rocket Engine Nozzle CFD Simulation Training
Beginner, Intermediate
Price: $20
In this project, the airflow entrance to a 2D convergent-divergent nozzle has been simulated, and the results of this simulation have been analyzed.
Hypersonic Combustion in Scramjet with Viscous Heating, CFD Simulation ANSYS Fluent Training
Intermediate, Advanced
Price: $36
The problem numerically simulates the Hypersonic Combustion in Scramjet with Viscous Heating using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software. The mesh type is Structured, and the element number equals 16320. We perform this simulation as unsteady (Transient). We use the Species Transport model to define the combustion process.
Price: $31.50
In this project, a NACA0012 Airfoil with the RBF (Mesh Morphing) Method has been simulated, and the results of this simulation have been investigated.
Price: $28
Simulation of Inviscid Supersonic Flow Over F-16 Aircraft. CFD Analysis of High Much Flow. Steady State CFD Simulation. Using Fluent Meshing Software for Mesh Generation.
Aerospike CFD Simulation Considering Shock Wave
Intermediate
Price: $20
The problem numerically simulates an Aerospike Considering Shock Wave using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. Mesh grid is generated using ANSYS Meshing, and the element number equals 153,987. k-Omega SST turbulence model is used to capture the shock wave.
Price: $96
In this project, we intend to simulate the NACA0012 airfoil with the compressible flow around it to compare and validate the results with the results in the article.
Price: $72
The problem numerically simulates the Wet Steam for Condensation inside a Steam Ejector using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software. The mesh type is Structured, and the element number equals 25984. We use the Wet Steam multiphase model to define Condensation. We use the VOF Multiphase model to define water and air. We use the Density-based solver to consider a compressive vacuum.