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: $89
Advance your compressible flow CFD skills with this 10-project ANSYS Fluent training package — covering compressible aerodynamics fundamentals, propulsion and compression machinery, and turbine and steam systems.
Compressible Flow: Intermediate CFD Training Package
Intermediate
Price: $49
Build intermediate-level expertise in compressible flow CFD with this 10-project ANSYS Fluent training package — covering shock waves and supersonic projectile motion, supersonic military aircraft, intake and compression devices, and advanced hypersonic and solver-comparison topics.
Price: $39
Compressible Flow: Beginner CFD Training Package is a ten-project introduction to high-speed and compressible-flow simulation in ANSYS Fluent. Starting from compressible flow over airfoils and building through transonic wings, internal nozzle flows, shock waves, and supersonic propulsion devices to a full aircraft geometry, it gives newcomers a hands-on, application-driven foundation in the CFD techniques behind modern aerospace and high-speed flow engineering — one real engineering case at a time.
Price: $56
This study investigates the aerodynamic performance of a turbine vane using CFD simulations with two different turbulence models The simulations were conducted using ANSYS Fluent, comparing the k-Omega SST and Large Eddy Simulation (LES) turbulence models The geometry of the turbine vane was created using ANSYS Design Modeler. The computational domain was then discretized using ANSYS Meshing, resulting in a high-resolution structured mesh of 12,634,415 elements
Price: $31.50
The problem numerically simulates the Lockheed Martin F-22 Raptor using ANSYS Fluent The geometry is designed in SpaceClaim, and the meshing is performed using fluent Meshing. The mesh type is polyhedral, and the element number equals 4,989,000. We aim to Maximize the Lift-to-Drag Ratio of wings. We use the Adjoint Solver to analyze the Shape Sensitivity. The Design Optimization is performed with the Gradient-based Radial Basis Function (RBF) used to apply Mesh Morphing.
Lockheed C-5 Galaxy Aerodynamic CFD Simulation
Beginner, Intermediate
Price: $10
This problem simulates a Lockheed C-5 Galaxy using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using fluent Meshing with approximately 14 million cells. The simulation is carried out using the pressure-based solver. The turbulence model is set to Realizable k-ε.
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.
Steam Turbine CFD Simulation, ANSYS Fluent Tutorial
Intermediate
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.
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.