Compressible Flow Online Courses

Price: $30

This problem simulates a F-22 aircraft using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using FLUENT Meshing. The simulation is carried out using the density-based solver. The turbulence model is set to k-ε Realizable.

Price: $56

This study investigates the flow dynamics in a steam turbine using CFD analysis in ANSYS Fluent. The 3D geometry was created in SpaceClaim and meshed using ANSYS Meshing, resulting in about 19 million tetrahedral elements. The simulation utilizes the Realizable k-ε turbulence model with standard wall function and includes the energy equation for temperature analysis. A density-based solver with real-gas-peng-robinson model is employed for compressible flow.

Price: $330

This project investigates the combustion process in a cylindrical chamber with a porous medium using CFD analysis in ANSYS Fluent. The geometry was designed in ANSYS Design Modeler and meshed using ANSYS Meshing, resulting in a high-quality mesh with 815,135 elements. The simulation employs the RNG k-ε turbulence model, Discrete Ordinate (DO) radiation model, and Species Transport model with Volumetric Reactions. Additional submodels for NOx and Soot formation are included. A cylindrical porous zone with 0.5 fluid porosity is incorporated near the inlet. The study demonstrates the impact of the porous medium on flow patterns, temperature distribution, species concentrations, and pollutant formation.

Price: $64

This project investigates turbocharger performance using CFD analysis in ANSYS Fluent, focusing on the fluid flow and thermal behavior of air through a one-sixth periodic sector of the geometry. The geometry was prepared using Vista CCD and BladeGen, and the mesh was generated with TurboGrid as a structured grid containing 972,176 cells. A pressure-based solver with the SST k-ω, k-ω turbulence model was used, and blade rotation was simulated at 92,000 RPM with the Frame Motion approach. The results highlight the influence of geometry on flow patterns, pressure distribution, and temperature gradients, offering insight into compression efficiency and overall turbocharger performance.

Price: $14

This project investigates the aerodynamic performance enhancement of an airfoil through CFD analysis in ANSYS Fluent. Three configurations are studied: a clean airfoil, an airfoil with a slat, and an airfoil with both slat and flap. The geometry was designed in ANSYS Design Modeler and meshed using ANSYS Meshing, resulting in approximately 5 million elements. The simulations use a density-based solver to account for compressibility effects. The study demonstrates significant improvements in lift-to-drag ratio, particularly when both slat and flap are employed.

Price: $16

This project simulates Noise Reduction Using Chevron Nozzles in Jet Engines using ANSYS Fluent. The geometry was created in SpaceClaim, and a mesh consisting of 1,317,762 elements was generated using ANSYS Meshing. The broadband noise source model was chosen to simulate noise generation and propagation.

Price: $14

The problem numerically simulates a Bluff Body Surface Heating on a Reentry Mission in ANSYS Fluent software. The geometry of the model is created using the Design Modeler software. The model is meshed in ANSYS Meshing, creating a structured mesh with 672,515 elements. The K-ω SST model is used to describe the turbulence of the flow.

Price: $12

The problem numerically simulates a Steam Ejector with Gas Methane Fluid in ANSYS Fluent software. The 2D geometry of the model is created in Design Modeler software. The model is meshed in ANSYS Meshing creating 11,132 elements. We simulate the problem via Density-based solver to define Compressible flow.

Price: $80

In this project, a solid fuel ramjet (SFRJ) engine has been numerically simulated by ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We Mesh the model with ANSYS Meshing software. The mesh type is Structured, and the element number equals 35,224. We use the Species Transport model to define the combustion process.