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.
Compressible Flow around an Aerial Structure by LES
Intermediate
Price: $56
The problem numerically simulates the compressible flow around an aerial structure 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 5515041. We perform this simulation as unsteady (Transient). We use the Density-based solver to define the compressible flow.
Rampressor, ANSYS Fluent CFD Simulation Training
Intermediate
Price: $36
The present problem simulates the air compression inside a Rampressor using ANSYS Fluent software.
Price: $32
The present project's results are compared with the experimental results of the paper “Midspan Flow-Field Measurements for Two Transonic Linear Turbine Cascades at Off-Design Conditions”. Turbulence modeling and Computational procedures (boundary conditions, etc.) are simulated based on the article “Numerical study of the flow field through a transonic linear turbine cascade at design and off-design conditions”.
Price: $16
The problem numerically simulates Compressible Flow in a 3-D Convergent-Divergent Nozzle using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software, and the element number equals 898906. We use the Ideal Gas option for air density to define the Compressible flow.
Acoustic in a Turbojet Intake Fan CFD Simulation
Intermediate
Price: $60
The problem numerically simulates Acoustic in a Turbojet (Intake Fan) 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 3723166. We use the Density-based solver to consider compressible flow. We use the Frame Motion (MRF) to define the rotational movement. We use the Broadband Noise Sources model to define the Acoustic model.
Steam Ejector in Refrigeration Cycle, Paper Validation
Intermediate, Advanced
Price: $270
The problem numerically simulates Steam Ejector in Refrigeration Cycle using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We Mesh the model with ANSYS Meshing software. The mesh type is Structured, and the element number equals 51990. This project is simulated and validated with a reference article. We use the Density-based solver to define Compressible flow.
Price: $20
The problem numerically simulates a wind tunnel using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software, and the element number equals 179542. We use the Density-Based solver to define the compressible flow.
Axial Flow Compressor (Rotor NASA 37) Simulation
Beginner, Intermediate
Price: $24
The problem numerically simulates Axial Flow Compressor using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software, and the element number equals 278162. We use a Density-Based solver to define the compressible flow. We use Frame Motion to define rotational motion around compressor blades.
Shock Wave in a Supersonic Airflow, Transient Solver
Intermediate
Price: $36
The problem numerically simulates Shock waves in a Supersonic Airflow using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software, and the element number equals 4466857. We perform this simulation as unsteady (Transient). We use the Density-Based solver to define the compressible flow.
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.