Compressible Flow Golden Training Package
Price:
$2,628
$1,369
The Compressible Flow GOLDEN Training Package delivers 45+ ANSYS Fluent tutorials, transforming teams into experts with instant project readiness. Tailored for professors, CEOs, and firms, it covers subsonic to hypersonic aircraft, shock waves, convergent-divergent, rocket, and aerospike nozzles, ramjets and scramjets, turbojet and turboprop engines, multi-stage compressors and turbines, steam ejectors with wet steam condensation, vortex tubes, reentry heating, and pressure-based versus density-based solvers. Includes step-by-step exercises, 1-year support, 3-month HPC, lifetime updates, and 15 years of MR CFD expertise for stress-free onboarding and competitive edge.
Compressible Flow Golden Training Package
Price:
$2,628
$1,369
The Compressible Flow GOLDEN Training Package delivers 45+ ANSYS Fluent tutorials, transforming teams into experts with instant project readiness. Tailored for professors, CEOs, and firms, it covers subsonic to hypersonic aircraft, shock waves, convergent-divergent, rocket, and aerospike nozzles, ramjets and scramjets, turbojet and turboprop engines, multi-stage compressors and turbines, steam ejectors with wet steam condensation, vortex tubes, reentry heating, and pressure-based versus density-based solvers. Includes step-by-step exercises, 1-year support, 3-month HPC, lifetime updates, and 15 years of MR CFD expertise for stress-free onboarding and competitive edge.
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.
Steam Ejector with Gas Methane Fluid CFD simulation, ANSYS Fluent
Intermediate, Advanced
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.
Solid Fuel Ramjet Engine, SFRJ, CFD Simulation, ANSYS Fluent
Intermediate, Advanced
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.
Vortex Tube CFD Simulation, ANSYS Fluent Training
Intermediate
Price: $30
This project numerically simulates the Vortex Tube using ANSYS Fluent software. The 3-D geometry is designed in Space Claim software. We used Fluent Meshing Software to generate mesh; the element number equals 497,635. Turbulent flow is modeled with the Spalart Almaras model. The solver is Density-Based and the Sutherland model is used for viscosity.
AK-47 Bullet CFD Simulation by ANSYS CFX, Training
Beginner, Intermediate, Advanced
Price: $120
The problem numerically simulates the AK-47 movement using ANSYS CFX software. The geometry is designed in a 3D model with the SpaceClaim software. We performed the mesh of the model with ANSYS Meshing software, and the element number equals 3,236,698. The High Speed (Compressible) Wall Heat Transfer Model option is enabled due to the compressibility of the air.
Multi-Stage Axial Compressor CFD Simulation
Intermediate
Price: $48
The problem numerically simulates a Multi-Stage Axial Compressor using ANSYS Fluent software. We design the 3-D model with the ANSYS Blade Gen. The meshing of the present model has been generated by TurboGrid software and the total cell number is 11,430 elements. The compressor motion has been modeled with the MRF method. The Turbo Workflow module was used to model the Compressor.
The Compressible Flow GOLDEN Training Package is MR CFD’s most complete ANSYS Fluent collection for high-speed and compressible-gas simulation, with 40+ hands-on tutorials that take you from first setup to advanced, publication-level modeling. Built for professors, CEOs, research teams, and engineering firms, it gives your group a ready-to-use project library, so new members become productive quickly and ongoing work starts from proven templates.
Shocks, nozzles, and external aerodynamics: Simulate transient shock waves in supersonic airflow, 3D convergent-divergent nozzles, supersonic nozzle flow separation, rocket engine nozzles, and aerospike nozzles. Study transonic NACA 0012 airfoils with paper validation, RBF Morph optimization, and slat and flap effects, plus supersonic flow over the F-16, F-35, F-22, SR-71 Blackbird, and C-5 Galaxy. Compare pressure-based and density-based solvers on F1 aerodynamics, and model wind tunnels and LES flow around aerial structures.
Air-breathing and high-speed propulsion: Explore ramjet design and combustion optimization, solid fuel ramjets, hypersonic scramjet combustion with viscous heating, supersonic jet ramped intakes, rampressors, turboprop propellers, and turbojet intake fan acoustics. Add chevron nozzle noise reduction on jet engines.
Turbomachinery: Analyze multi-stage axial compressors and gas turbines, NASA Rotor 37, transonic turbine cascades at off-design conditions (paper validation), steam turbines, turbine vanes with LES and k-omega SST, and turbochargers built with BladeGen and TurboGrid.
Ejectors, condensation, and thermal devices: Model steam ejectors in refrigeration cycles, methane steam ejectors, wet steam condensation inside ejectors, and vortex tubes.
Special applications: Simulate bluff body surface heating on a reentry mission, bullet flight with dynamic mesh, and compressible flow in a bent pipe.
What’s included:
Step-by-step exercises with complete setup, meshing, solving, and post-processing
Projects spanning beginner, intermediate, and advanced levels, including paper-validation cases
1-year technical support
3-month HPC access
Lifetime updates
Backed by 15 years of MR CFD simulation expertise
Whether you’re preparing a research paper, optimizing a nozzle or engine component, or building in-house CFD capability, this package gives you the knowledge, tools, and confidence to deliver faster and stay ahead of the competition.