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


About this gig
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.
Delivery style preference
Please inform the freelancer of any preferences or concerns regarding the use of AI tools in the completion and/or delivery of your order.
Get to know Michael Howe
Professional Aerodynamic Engineer
- FromUnited States
- Member sinceJul 2026
- Avg. response time1 hour
Languages
English
Other Industrial & Product Design Services I Offer
FAQ
What do you need from me to start?
Mission requirements: payload, wingspan/weight limits, cruise speed, target endurance, and expected Reynolds number range. If you don't have these defined yet, I'll help derive them from your mission profile before running any analysis.
Is XFLR5/Flow5 accurate enough, or will I need CFD too?
XFLR5 uses XFoil's viscous panel method for 2D airfoil polars and VLM for 3D wing analysis — reliable for early-stage sizing, stability derivatives, and attached-flow performance. Past stall, at high-Re turbulent transition, or in compressible regimes, panel methods lose accuracy.
Can you start from just an idea, with no CAD or geometry yet?
Yes. I build the airfoil, planform, and empennage sizing directly from your mission spec, or refine an existing .xfl file or geometry you already have.
