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Aerodynamic Analysis of GOE398 Airfoil | Ansys Fluent

Overview This project consists of a computational fluid dynamics (CFD) analysis of the GOE398 airfoil using Ansys Fluent. The objective was to evaluate the airfoil’s aerodynamic behavior at various angles of attack under steady-state conditions. The study includes pressure and velocity fields, as well as lift and drag coefficient. The results were included in a presentation at the XVII Ansys Convergence Mexico 2020, focused on basic aerodynamic analysis. Methodology The airfoil profile was modeled in 2D. Simulations were performed for angles of attack between 0° and 20°. A structured mesh was generated and refined near the boundary layer. Analysis Parameters Pressure coefficient distribution Velocity magnitude and streamlines Lift and drag coefficient estimation Stall onset and boundary layer behavior Tools and Technologies Simulation: Ansys Fluent

  • CFD
  • Ansys
  • Aerodynamics
  • Fluent
  • Engineering
Monday, January 1, 2024 | 1 minute Read
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Cloud Surfer 2022 | Aerodesign

Overview Cloud Surfer 2022 was a radio-controlled cargo aircraft developed as part of the SAE Aerodesign Mexico competition. The project focused on aerodynamic optimization, structural feasibility, and payload integration within competition constraints. Tools and Technologies SolidWorks for 3D modeling Ansys Fluent for CFD simulation XFLR5 for preliminary aerodynamic analysis MATLAB for performance estimation Gallery

  • Aerodynamics
  • CAD
  • CFD
  • Aerospace
  • Engineering
Monday, January 1, 2024 | 1 minute Read
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RC Flying Wing | Aerodesign

Key Features Delta-wing flying configuration Brushless motor with rear propeller Elevon-based control system Lightweight foam construction RC electronics Technologies Used SolidWorks for CAD sketches Manual fabrication using foam and adhesives RC components (transmitter, receiver, ESC, motor, servos)

  • Aerodynamics
  • DIY
  • CAD Design
Monday, January 1, 2024 | 1 minute Read
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TEUS 2023 | SAE Aerodesign México

Overview TEUS 2023 was the aircraft designed and developed for participation in the SAE Aerodesign México national competition. The objective of the contest was to construct a remote-controlled aircraft capable of lifting a maximum payload under cargo dimensional and power consumption constraints. Contributions Designed the wing profile and internal structural frame using SolidWorks. Constructed and assembled the fuselage and propulsion elements. Performed motor–propeller characterization using a custom-built test bench. Participated in telemetry setup, weight distribution analysis, and test flights. Competed in the official SAE Aerodesign México 2023. Technologies Used SolidWorks for mechanical design Gallery

  • Aerodynamics
  • CAD Design
  • Embedded Systems
Monday, January 1, 2024 | 1 minute Read
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Contact me:
  • jm.vargascruz@gmail.com
  • jmvargascruz
  • Jesus Vargas

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