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.

Audio: English
Subtitles: English, Spanish, Arabic, Turkish, French, Portuguese
Beginner, Intermediate, Advanced
48 Courses
22h 48m 45s
  • 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.

    Audio: English
    Subtitles: English, Spanish, Arabic, Turkish, French, Portuguese
    Beginner, Intermediate, Advanced
    48 Courses
    22h 48m 45s
    Buying this package gives you full access to every course below, including new courses added to this category in the future.

    Price: $36

    The problem numerically simulates the Hypersonic Combustion in Scramjet with Viscous Heating using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software. The mesh type is Structured, and the element number equals 16320. We perform this simulation as unsteady (Transient). We use the Species Transport model to define the combustion process.

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    Price: $31.50

    In this project, a NACA0012 Airfoil with the RBF (Mesh Morphing) Method has been simulated, and the results of this simulation have been investigated.

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    Price: $28

    Simulation of Inviscid Supersonic Flow Over F-16 Aircraft. CFD Analysis of High Much Flow. Steady State CFD Simulation. Using Fluent Meshing Software for Mesh Generation.

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    Price: $20

    The problem numerically simulates an Aerospike Considering Shock Wave using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. Mesh grid is generated using ANSYS Meshing, and the element number equals 153,987. k-Omega SST turbulence model is used to capture the shock wave.

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    Price: $96

    In this project, we intend to simulate the NACA0012 airfoil with the compressible flow around it to compare and validate the results with the results in the article.

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    Price: $72

    The problem numerically simulates the Wet Steam for Condensation inside a Steam Ejector 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 25984. We use the Wet Steam multiphase model to define Condensation. We use the VOF Multiphase model to define water and air. We use the Density-based solver to consider a compressive vacuum.

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    Price: $36

    In this project F1 Aerodynamics CFD Simulation is carried out using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. The Mesh is generated by ANSYS Meshing software, and the element number equals 1,253,296. Pressure-Based and Density-Based solvers are used in the simulation.

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    Price: $20

    The problem numerically simulates the F-35 Considering Compressible Flow using ANSYS Fluent software. We design the 3-D model with the CAD software. We mesh the model with ANSYS Meshing software, and the element number equals 1,845,364. We use the ideal gas to consider a compressible flow.

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    Price: $20

    The present problem simulates the airflow around the aircraft wing with a flap and slat, using ANSYS Fluent software.

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    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.