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Compressible Flow CFD Training Package, Beginners, 10 Projects

$360.00 Student Discount

Compressible Flow CFD Training Package is prepared for BEGINNER users of ANSYS Fluent software in the COMPRESSIBLE FLOW area, including 10 practical exercises.

Click on Add To Cart and obtain the Geometry file, Mesh file, and a Comprehensive ANSYS Fluent Training Video. By the way, You can pay in installments through Klarna, Afterpay (Clearpay), and Affirm.

If you decide to use PayPal to pay, you will get a 5% discount on your order.

To Order Your Project or benefit from a CFD consultation, contact our experts via email ([email protected]), online support tab, or WhatsApp at +44 7443 197273.

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If you want the training video in another language instead of English, ask it via [email protected] after you buy the product.

Steam Ejector ANSYS Fluent CFD Simulation Tutorial

  • 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.

 

NACA 0012 Airfoil, Compressible Flow CFD Simulation

  • 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.

Supersonic Nozzle Flow Separation and Shock Wave

  • The problem numerically simulates the performance of phase change materials (PCM) in a storage tank using ANSYS Fluent software.
  • 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.

Shock Wave in a Supersonic Airflow, Transient Solver

  • 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.

 

Wind Tunnel CFD Simulation, Compressible Flow, ANSYS Fluent Tutorial

  • 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.

Compressible Flow in 3-D Convergent-Divergent Nozzle

  • 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.

F-35 Considering Compressible Flow, ANSYS Fluent CFD Simulation Training

  • 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.

Slat and Flap Devices Effects on an Aircraft Wing

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

Drone CFD Analysis in Low and High Altitudes, ANSYS Fluent Simulation Training

In this study, the effect of different altitudes of a high-speed drone has been studied using ANSYS Fluent software.

Axial Flow Compressor (Rotor NASA 37) Simulation

  • 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.

Special Offers For All Products

If you need the Geometry designing and Mesh generation training video for all the products, you can choose this option.
The journal file in ANSYS Fluent is used to record and automate simulations for repeatability and batch processing.
Editable geometry and mesh allows users to create and modify geometry and mesh to define the computational domain for simulations.
The case and data files in ANSYS Fluent store the simulation setup and results, respectively, for analysis and post-processing.
Geometry, Mesh, and CFD Simulation methodologygy explanation, result analysis and conclusion

Special Offers For Single Product

If you need the Geometry designing and Mesh generation training video for one product, you can choose this option.
If you need expert consultation through the training video, this option gives you 1-hour technical support.
The journal file in ANSYS Fluent is used to record and automate simulations for repeatability and batch processing.
editable geometry and mesh allows users to create and modify geometry and mesh to define the computational domain for simulations.
The case and data files in ANSYS Fluent store the simulation setup and results, respectively, for analysis and post-processing.
Geometry, Mesh, and CFD Simulation methodologygy explanation, result analysis and conclusion
The MR CFD certification can be a valuable addition to a student resume, and passing the interactive test can demonstrate a strong understanding of CFD simulation principles and techniques related to this product.
Enhancing Your Project: Comprehensive Consultation and Optimization Services

Description

Compressible Flow CFD Simulation Package, 10 ANSYS Fluent Training for BEGINNER Users

Compressible Flow CFD Training Package is prepared for BEGINNER users of ANSYS Fluent software in the COMPRESSIBLE FLOW area, including 10 practical exercises. You will learn and obtain comprehensive training on how to simulate projects. The achieved knowledge will enable you to choose the most appropriate modeling approaches and methods for applications and CFD simulations.

Compressible Flow occurs in many industrial devices and applications. Some of these cases are investigated in this training package.

Steam Ejector

Problem 1 deals with the flow of water vapor as the main fluid (primary) and the secondary fluid (suction) within a convergent-divergent Steam Ejector. The purpose of the present simulation is to investigate the behavior of primary and secondary fluid after passing through the internal convergent-divergent nozzle and the ejector diffuser. In the present model, due to the vacuum pressure difference between the two inlet fluids, the suction phenomenon for the secondary fluid has to occur.

Airfoil, Wing, and Airplane

Project 2 is going to simulate a NACA 0012 airfoil in the compressible airflow field. Geometric defining parameters include chord line, angle of attack, leading edge, and trailing edge. The direction of the airflow into the airfoil body is defined by the angle of attack (the angle between the chord and the horizontal direction of the airflow velocity).

Problem 3 simulates the airflow around the aircraft wing with a flap and slat. In this project, a 3D airplane wing is designed; In such a way a Flap is on the trailing edge, and a Slat is on the wing’s leading edge.

Project 4 is going to study a Supersonic Compressible Flow adjacent to an F-35 plane. The geometry is a 20-meter F-35 plane inside a 150-meter wind tunnel. The air is considered a compressible ideal gas, and the Mach number of 2.0 was achieved at the maximum speed of 544 m/s.

In study 5, the effect of different altitudes of a high-speed DRONE has been studied. The fluid is air, and we considered it as a compressible ideal gas. The maximum speed of the drone is 30 m/s, and the investigated altitudes are 20m and 2000m as low and high altitudes, respectively.

Shock Wave in Supersonic Airflow (Compressible Flow)

Problem 3 simulates the supersonic airflow encountered by a two-way oblique airfoil barrier passing through a channel, thus investigating fluid behavior and creating a shock wave phenomenon. The airflow in the simulation environment around the obstacles and canals has a temperature of 129.46 Kelvin and a Mach number of 2.49, and the direction of the airflow is generally assumed to be in the same direction. Mach number is a non-dimensional number that indicates the ratio of fluid velocity to sound velocity in the same fluid.

Nozzle

Study 4 simulates airflow within a supersonic convergent-divergent nozzle and examines the behavior of airflow separation from the nozzle in the surrounding environment. In order to simulate the present model, the pressure condition in the nozzle input section (pressure-inlet condition) and the ambient output sections (pressure-outlet condition) have been used. The nozzle pressure ratio (NPR) is equivalent to the ratio of the inlet air pressure of the nozzle to the ambient pressure.

In Project 5, the airflow will enter the convergent-divergent nozzle with a pressure of 70 bars and a Mach number of 0.2 with a temperature of 2735 K. After passing the throat zone. The airflow will gain speed and lose its temperature as it passes through the diffuser.  The standard k-epsilon model with standard wall function is used to solve fluid flow equations. The energy model is activated, and the ideal gas equation is exploited to calculate the density changes in the computational domain.

Wind Tunnel

The wind tunnel is one of the most widely used aerodynamic testing devices today.

In project number 6, a wind tunnel and a specific body that is placed inside it are modeled. The effect of drag force on this body is investigated. The energy model and standard k-epsilon model with the use of standard wall functions are activated.

Compressor (Compressible Flow)

Finally, problem 10 is going to simulate the airflow inside an axial flow compressor (Rotor Nasa 37). The present model consists of a series of blades for an axial flow compressor connected to the central axis within a cylindrical area. To simplify the simulation model, only one row of rotating blades is drawn on the central rotor of the compressor.

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Reviews

  1. Avatar Of Ms. Jazmyn Hintz Sr.

    Ms. Jazmyn Hintz Sr.

    Hey, I’ve got a specific simulation I want to do. Can you guys handle custom requests?

    • Avatar Of Mr Cfd Support

      MR CFD Support

      Totally, we’re all for your ideas and we’re ready to tweak our simulations to fit what you need. Just spill the beans on the simulation you’re thinking about, and we’ll do our best to help you out.

  2. Avatar Of Madeline Nolan

    Madeline Nolan

    I’m interested in aerospace applications. Does this package cover supersonic and hypersonic flows?

    • Avatar Of Mr Cfd Support

      MR CFD Support

      Yes, this training package includes exercises that cover a wide range of flow regimes, including subsonic, transonic, supersonic, and hypersonic flows. This makes it particularly useful for aerospace applications.

  3. Avatar Of Sydni Rice

    Sydni Rice

    I see that this training package uses the density-based solver. Can you explain why this solver is suitable for compressible flows?

    • Avatar Of Mr Cfd Support

      MR CFD Support

      The density-based solver is ideal for compressible flows as it directly solves the conservation equations of mass, momentum, and energy. This allows it to accurately capture shock waves and other phenomena typically associated with compressible flows.

  4. Avatar Of Mr. Davin Rowe

    Mr. Davin Rowe

    Can this training package help me understand the effects of Mach number on flow characteristics?

    • Avatar Of Mr Cfd Support

      MR CFD Support

      Absolutely! The exercises included in this package are designed to provide a comprehensive understanding of compressible flows, including the effects of varying the Mach number. You will gain insights into how changes in the Mach number can affect flow characteristics such as pressure, temperature, and density.

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