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.
Supersonic Nozzle Flow Separation and Shock Wave
Beginner, Intermediate
Price: $16
The present study simulates Supersonic Nozzle Flow Separation within a supersonic convergent-divergent nozzle. We design the 2-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software, We use a Density-Based solver to define the compressible flow. The mesh type is Structured, and the element number equals 9000.
NACA 0012 Airfoil, Compressible Flow CFD Simulation
Beginner, Intermediate
Price: $20
The problem numerically simulates NACA 0012 Airfoil (Compressible Flow) using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing. The model mesh is structured, and 35000 cells have been created. We apply a Density-based solver to define the compressible flow. We determine the Mach number for the inlet boundary condition.
Steam Ejector ANSYS Fluent CFD Simulation Tutorial
Beginner, Intermediate
Price: $20
The present problem deals with the flow of water vapor as the primary fluid and the secondary fluid within a steam ejector by ANSYS Fluent software. We design the present 2-D model by the Design Modeler software. Meshing was performed by ANSYS Meshing software. The mesh type is structured, and the element number equals 51990. We have used a density-based solver due to the compressibility in this project.
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.