I will design and perform uav aerodynamic analysis using xflr5 and flow5

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michael_howe2
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michael_howe2
Michael Howe
Algumas informações são exibidas no idioma inglês.
design and perform uav aerodynamic analysis using xflr5 and flow5
Tela Inteira
design and perform uav aerodynamic analysis using xflr5 and flow5

Sobre este Serviço

Struggling to get accurate aerodynamic data for your UAV or aircraft design?

You've found the right gig.


I specialize in UAV design and aerodynamic analysis using XFLR5, Flow5, and CFD methods helping drone developers, students, and startups turn design ideas into validated, flight-ready aircraft.


What you'll get:

  • Full UAV / fixed-wing aircraft aerodynamic design
  • Airfoil selection and performance analysis (Cl, Cd, Cm, L/D)
  • XFLR5 and Flow5 simulation, analysis, and reports
  • Wing, tail, and fuselage sizing and optimization
  • Stability and performance analysis
  • Clean documentation with clear 3-view drawings
  • Fast communication and revisions until satisfied


Why work with me:

I don't just hand you numbers I explain what the results mean and how they shape your design decisions, so you can build on your work with confidence. Every project gets the attention to detail I'd want on my own aircraft.


If you're finishing a thesis, developing a commercial drone, or need aerodynamic validation for a client project, I deliver precise, professional results on time, every time.


Message me before ordering so we can discuss your project and get the best outcome.

  • Tipo de entrega

    • Arquivo Digital

  • Materiais

    • Metal

  • Área de Especialização

    • Aeroespacial
    • Máquinas
    • Peças mecânicas

  • Software de Design

    • Catia
    • Fusion 360
    • Solidworks
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Conheça mais sobre Michael Howe

Michael Howe

Professional Aerodynamic Engineer

  • A partir deEstados Unidos
  • Membro desdejul. de 2026
  • Responde em aprox.:1 hora

  • Idiomas

    Inglês
We're an aerodynamic engineering team specializing in UAV design using XFLR5, Flow5, and CFD methods. From mission requirements payload, endurance, Reynolds number, we derive airfoil selection, wing design, and stability analysis, then validate lift, drag, and control derivatives before you build anything. Every project ships with a documented methodology report, built to be defended in a thesis review or client meeting. If your project needs real aerodynamic engineering, message us.

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