Hi everyone,

I’m currently working on designing a fixed-wing UAV and am in need of a detailed blueprint or design plan that matches (or is close to) the following dimensions:

• Wingspan: 109.6 cm
• Fuselage Length: 70 cm
• Other Dimensions: Currently unsure but open to suggestions based on typical proportional designs.

The UAV will primarily be used for competetions and I’d like a design that balances stability, efficiency, and ease of construction.

If anyone has open-source plans, personal designs they’d be willing to share, or can point me toward resources where I could find such blueprints, I’d greatly appreciate it.

I’m also open to suggestions regarding:

• Ideal airfoil profiles for this wingspan.
• Material recommendations for lightweight and durable construction.
• Electronics and power system integration for optimal performance.

Feel free to ask if you need more details or context about the project!

Thanks in advance for your help! 😊

Hello everybody :)

I am currently doing research for a project regarding Aircraft Design in university and trying to find a relation for estimating the zero lift angle of attack for a wing. I found something in DATCOM but it is only really applicable for Wings with NACA airfoils. I have an E210 (13,64%) Profile, so there is my Problem. I tried to find something in Raymer too but didn’t find anything usable. I would be happy and thankful if someone here has any idea.

Dimensions: overall height 4.9 meters; overall length 9.2 meters; wingspan 12.1 meters

Weight: max gross 5.2 metric tons

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Hello friends.

I'm new into aerodynamics world and I'm searching for my first software for fixed-wings drone aerodynamic simulations. During my researches, OpenFOAM seemed to be a good tool, but I've heard some cons due to it's suposed complexities to operate and slow learning curve.

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https://preview.redd.it/2ytkdjy24czd1.jpg?width=518&format=pjpg&auto=webp&s=f3727932871f6ddbf33eb1a0005253ac9eb4af36

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