telnar1236
Elite member
You might need to look at your boundary conditions, mesh, and assumptions for the simulation. This plane does look a bit small for a 750g weight, but it should still be producing more than 275g of lift. One big thing to consider is that the plane will fly at a positive angle of attack. At 0 AOA, a symmetrical airfoil will also produce 0 lift. However, at a higher AOA, a delta will produce a ton of lift as it generates a powerful leading-edge vortex keeping the flow attached. It's also almost impossible to get good results for a delta wing without control surface deflection since that deflection kills part of the lift, or with canards adds to it.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!
For preliminary work, xflr5 is a good resource that can give you reliable results without needing to go the whole CFD route.
xflr5
www.xflr5.tech
In terms of CFD, Solidworks simulation is also pretty poor. Solidworks is mostly a piece of CAD software, so any results you get should be taken with a grain of salt.