Paramotor, Ansys Fluent CFD Simulation Training

$150.00 Student Discount

In this project, a flow in a paramotor has been simulated, and the simulation results have been investigated.

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.

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.

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.


 Paramotor Project Description

The present simulation is about a paramotor in a paraglider via ANSYS Fluent. A paramotor is the propulsion part of a paraglider that attaches to the pilot’s seat. These engines are powered by gasoline and have fan blades attached to them. This simulation defines a cylindrical computational domain for airflow with a temperature of 26.85 C. For inlet and outlet boundaries of this domain, a pressure boundary condition is defined to determine the direction of air movement according to the amount of pressure. In the middle part of this model, a surface is defined as a fan, and the fan boundary condition with 383.8-pascal pressure jump is used. The aluminum casing of the engine with its thermocouple is defined behind the fan; It is assumed that the inner wall inside the engine has a constant temperature equal to 157 C. It is assumed that this temperature is defined based on the heat generated by the combustion inside the engine.

Geometry & Mesh

The present model is designed in the 3D model via Design Modeler. This model includes a domain designed with a fan in the middle. The following figure shows the geometry of the model.

The mesh of the present model has been done via ANSYS Meshing. Mesh is done unstructured, and the number of cells equals 1550207. The following figure shows the mesh of the model.


Paramotor Set-Up & Solution

Assumptions used in this simulation  :

  • Pressure-based solver is used.
  • The present simulation is steady.
  • The effect of gravity is ignored.
Viscous k-epsilon
Near-wall standard
near wall treatment standard wall function
Energy On
Boundary conditions
Inlet Pressure Inlet
gauge total pressure 0 pascal
total temperature 26.85 C
Inner Wall of the Thermocouple Wall
wall motion stationary wall
thermal conditions coupled
Inner Wall Wall
temperature 157 C
Outlet Pressure Outlet
gauge pressure 0 pascal
Fan Fan
pressure jump profile 383.8 pascal
Symmetry Wall Symmetry
Pressure-Velocity Coupling SIMPLE
pressure Second-order
momentum Second-order upwind
turbulent kinetic energy First-order upwind
turbulent dissipation rate First-order upwind
energy Second-order upwind
Initialization methods standard
gauge pressure 0 pascal
velocity (x,y,z) 0 m.s-1
temperature 26.85 C

Paramotor Results

After the solution, 2D and 3D temperature, velocity, and pressure contours are obtained. The contours show that airflow passes through the fan, air velocities increase, and significant pressure differences appear. Around the engine, local temperature increases due to the temperature of the inner wall inside the engine appearing. The results are shown in Figures 3 to 9.


  1. Lucious Carroll

    Does the training include any material on optimizing the design of a paramotor?

    • MR CFD Support

      Absolutely. The training includes a section on design optimization. This is crucial in improving the performance and efficiency of your paramotor design.

  2. Lenore Barrows

    How does this training handle the complexities of simulating the interaction between the paramotor and the pilot?

    • MR CFD Support

      The training includes a section on simulating the interaction between the paramotor and the pilot. This is a complex aspect of paramotor simulation and the training is designed to help you understand and simulate it effectively.

  3. Mr. Napoleon Oberbrunner

    Can this training help me understand the impact of different weather conditions on the flight of a paramotor?

    • MR CFD Support

      Yes, it can. The training includes exercises that explore the impact of different weather conditions, such as wind speed and direction, on the flight of a paramotor.

  4. Katrina Spinka PhD

    Does the training cover how to set up boundary conditions for a simulation?

    • MR CFD Support

      Absolutely. The training includes a comprehensive section on setting up boundary conditions. This is an essential step in setting up a successful simulation.

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