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Aerodynamic and Aerospace Training Package, Intermediates, 10 Projects

Original price was: $1,180.00.Current price is: $390.00. Student Discount

This training package includes 10 practical aerodynamic and aerospace engineering exercises using ANSYS Fluent software.

Click on Add To Cart and obtain the Geometry file, Mesh file, and a Comprehensive ANSYS Fluent Training Video.

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.

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.

Sound Generation on an Airfoil, 3 Different Attack Angles

  • The problem numerically simulates the Sound Generation on Airfoil 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 231840.
  • This project has been done in three modes with different angles of attack for airfoils.
  • We use the Broadband Noise Sources model to define the Acoustic model.

Helicopter CFD Simulation, ANSYS Fluent Training

  • The problem numerically simulates the Helicopter 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 937677.
  • We perform this simulation as unsteady (Transient).
  • The Mesh Motion option is used to define the rotating motion of helicopter blades.

Movement of Golf Ball, Impact (Dynamic Mesh), ANSYS Fluent Simulation Tutorial

  • The problem numerically simulates the Movement of a Golf Ball using ANSYS Fluent software.
  • We design the 3-D model by the Design Modeler software.
  • We mesh the model with ICEM software, and the element number equals 945765.
  • We perform this simulation as unsteady (Transient).
  • We use the Dynamic Mesh model to define the motion of the golf ball within the domain.

 

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.

Sound Generation on a Car with and without Spoiler

  • The problem numerically simulates Sound Generation (Acoustic) on Audi Car with and without Spoiler using ANSYS Fluent software.
  • We design the 3-D model by the Design Modeler software.
  • We Mesh the model by ICEM software.
  • We use the Broadband Noise Sources model to define the Acoustic model of the present work.
  • We aim to study changes in acoustic power level (dB) or sound pressure in the present work.

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.

Aircraft Propeller CFD Simulation Using Mesh Motion, ANSYS Fluent Training

  • The problem numerically simulates the Aircraft Propeller 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 692023 and 3812519.
  • We perform this simulation as unsteady (Transient).
  • We use the Mesh Motion model to define the rotational movement.
  • We study aerodynamic forces, including drag and lift.

 

F1 Aerodynamics CFD Simulation, Pressure-Based and Density-Based

  • 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.

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
If you want training in any language other than English, we can provide you with a subtitled video in your language.

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
Collaborative Development of a Conference Paper on Cutting-Edge Topics with MR CFD
Collaborative Publication Opportunity: Contribute to an ISI Article and Get Featured in Scopus and JCR-Indexed Journals
If you want training in any language other than English, we can provide you with a subtitled video in your language.

Description

Aerodynamic & Aerospace ANSYS Fluent CFD Simulation Training Package for INTERMEDIATE Users

This training package includes 10 practical aerodynamic and aerospace engineering exercises using ANSYS Fluent software. MR CFD suggests this package for all aerodynamic and aerospace engineers who will learn CFD simulation in this field at the INTERMEDIATE level.

Compressible Flow

In practical exercise, number 1, a wind tunnel and a specific body placed inside it are modeled considering compressible flow. The effect of drag force on this body is investigated. The energy model and standard k-epsilon model with standard wall functions are activated. Project number 5 will 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. Problem number 7 simulates the compressible 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.

In study number 8, the effect of different altitudes of a high-speed drone has been studied. The fluid is air, and we consider it 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, respectively.

Acoustic in Aerodynamic

Problem number 2 simulates sound pressure waves around an airfoil. This project examines the sound waves generated around the body of an airfoil. This project uses an acoustic model in Fluent software to simulate and analyze sound or acoustic waves. The Broadband Noise Sources model has also been used to define the type of acoustic model of the present work. Problem number 6 simulates sound pressure waves around an AUDI car with and without a spoiler. Aeroacoustics is a branch of acoustic science that investigates the production of Noise. In general, Noise can be generated by the movement of turbulent fluid or from collisions of aerodynamic forces with surfaces.

Moving Mesh (Mesh Motion) & Dynamic Mesh

In project number 3, the rotation of helicopter wings is simulated in transient time formulation, and the results, including net upward force, wing tip speed, and Tip Speed Ratio (TSR), is investigated. To generate upward movement in aerodynamic applications, movement of a certain amount of air in the downward direction is needed, generating upward motion. This air movement is done for helicopters using a propeller consisting of 2 or more wing-shaped geometries rotating around a center. In practical exercise number 4, a golf ball movement with an aerodynamic point of view has been studied applying Dynamic Mesh, the force applied to the ball is equal to 200 N. Due to the impact, the golf ball displacement has been studied in terms of time.

Project number 9 examines the analysis of thrust and lift forces behind the propeller on the fuselage. Aircraft and propeller modeling is performed in two zones rotational and stationary. The rotating computational domain must rotate around the impeller axis to model the impeller rotational motion using the Mesh Motion method.

Pressure-Based & Density-Based Solvers

Finally, In practical exercise number 10, the aerodynamic coefficients of a Formula One (F1) car by two different solvers, pressure-based and density-based, have been studied at a speed of 108 meters per second at a lateral angle of zero degrees (actually a straight path). This velocity at the ground level is equivalent to a Mach number of approximately 0.32. We know this area from Mach number is the transition zone from incompressible to compressible flow, so on this geometry, the drag coefficient is investigated using two pressure-based and density-based solvers is discussed.

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