I’m trying to model and 3D print a roughly 1-meter-long JAS 39 Gripen RC model for a school project. I’ve been researching online and working on the modeling process, but now that I’m trying to determine if it can actually fly, I’m struggling.
According to the simulations I’m running in SolidWorks, the model has no chance of getting off the ground. However, when I look at similar models on YouTube, it seems like mine should be able to fly. When I import the model into Bambu Studio, it estimates a weight of about 710g at 5% gyroid infill. Based on that, I’ve been roughly estimating the final weight to be between 1–1.5 kg.
The issue is that my flow simulations indicate almost no chance of achieving lift. With a convex airfoil, I’m only getting about 0.8N of lift at 15 m/s, which I doubt will be enough. To improve this, I redesigned the wings to have roughly twice the surface area, using a thicker and more aggressive airfoil. With this new design, I achieved 2.7N of lift under the same conditions. The original wing has a total area of 0.098 m², while the larger-winged version has 0.18 m².
I’m mainly looking for feedback from more experienced individuals on whether this model seems flyable. Additionally, I’d appreciate any suggestions on airfoil selection—what type to use or how to design one that suits my needs. Any advice, suggestions, or feedback would be greatly appreciated!
According to the simulations I’m running in SolidWorks, the model has no chance of getting off the ground. However, when I look at similar models on YouTube, it seems like mine should be able to fly. When I import the model into Bambu Studio, it estimates a weight of about 710g at 5% gyroid infill. Based on that, I’ve been roughly estimating the final weight to be between 1–1.5 kg.
The issue is that my flow simulations indicate almost no chance of achieving lift. With a convex airfoil, I’m only getting about 0.8N of lift at 15 m/s, which I doubt will be enough. To improve this, I redesigned the wings to have roughly twice the surface area, using a thicker and more aggressive airfoil. With this new design, I achieved 2.7N of lift under the same conditions. The original wing has a total area of 0.098 m², while the larger-winged version has 0.18 m².
I’m mainly looking for feedback from more experienced individuals on whether this model seems flyable. Additionally, I’d appreciate any suggestions on airfoil selection—what type to use or how to design one that suits my needs. Any advice, suggestions, or feedback would be greatly appreciated!