I will do aerodynamic analysis, airfoil and wing design with xflr5


About this gig
I analyze airfoils, wings and full aircraft in XFLR5 and deliver clear plots plus a plain-language recommendation, not just raw output.
WHAT YOU GET
- Airfoil selection and comparison (Cl, Cd, Cm vs angle of attack and Reynolds number)
- Wing planform study: aspect ratio, taper, sweep, twist
- Lift and drag polars, stall behavior and L/D
- Static stability, neutral point and CG range
- Stability and control derivatives for the full aircraft
- Result plots and a PDF report with recommendations
BEST FOR
Drones, RC and small aircraft, gliders and light aircraft at low to moderate speeds.
GOOD TO KNOW
XFLR5 uses panel and vortex-lattice methods, so it suits preliminary design. For high-fidelity 3D CFD, message me first and I'll scope it separately.
HOW IT WORKS
1. Send your flight conditions and a sketch, CAD or dimensions
2. I confirm scope
3. I deliver the plots, the report and the XFLR5 project file
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 Samran Hameed
Aerospce Project Manager
- FromPakistan
- Member sinceAug 2021
- Avg. response time1 hour
Languages
Urdu, English
My Portfolio
FAQ
Do I need a CAD file?
No. Dimensions, a sketch or a drawing are enough for XFLR5.
How accurate are the results?
They are suitable for preliminary design and for comparing options. XFLR5 is built for low-Reynolds-number flight, so it fits drones, gliders and light aircraft, and it is less reliable for drag-dependent derivatives. For higher fidelity, I can cross-check key cases with 3D CFD as a separate order.

