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.
Multi-Stage Axial Gas Turbine CFD Simulation
Intermediate
Price: $72
The problem numerically simulates a Multi-Stage Axial Gas Turbine 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 12,182 elements. The compressor motion has been modeled with the MRF method. The Turbo Workflow module was used to model the turbine.
Turboprop Engine Propeller CFD Simulation
Intermediate
Price: $14
The problem numerically simulates a Turboprop Engine Propeller using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software. The element number equals 9,622,423. Multiple Reference Frames (Frame Motion) are used to model the rotational motion of the propeller. The Density-Based solver is used.
Supersonic Jet Ramped Intake CFD Simulation Training
Intermediate
Price: $30
The problem numerically simulates the Supersonic Jet Ramped Intake using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software, and the element number equals 1278343. We have used the density-based solver due to the compressibility.
Ramjet Engine, Design and Combustion Optimization (SR-71 Blackbird), Industrial Application
Intermediate, Advanced
Price: $390
In this project, an industrial Ramjet Engine has been numerically simulated by ANSYS Fluent software. Studying Combustion, Mach Number, Pressure, Density (Compressible Flow), and Thermal analysis. Optimizing the Thrust number. Ramjet Design Improvement. RSM analysis applying DOE.
Price: $28
The problem numerically simulates the HPBT Bullet movement after firing using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. The Mesh is modeled by ANSYS Meshing software, and the element number equals 13,040. We perform this simulation as unsteady (Transient). The Dynamic Mesh method is used to simulate the movement process.
Compressible Flow in a Bent Pipe CFD Simulation
Beginner, Intermediate
Price: Free
The present CFD Project simulates Compressible Flow in a Bent Pipe via ANSYS Fluent software. We modeled the geometry using ANSYS Design Modeler software and created the mesh using ANSYS Meshing software. The number of cells after refinement is 1,450,983. The solution has been solved Transiently. The solver is Density-Based to capture the compressibility of the flow.
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.
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.