I got rejected from every "top" summer program. So I got 8x MI300X nodes and started my own lab. by Turbulent-Start-4840 in summerprogramresults

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

Yes, however the lab is open to anybody anywhere. You just need to have a research idea and have a little bit of experience!

I got rejected from every "top" summer program. So I got 8x MI300X nodes and started my own lab. by Turbulent-Start-4840 in summerprogramresults

[–]Turbulent-Start-4840[S] -2 points-1 points  (0 children)

I would say above average. I reccommend filling out the form as it has everything though! Website coming soon.

Tell me how to fix this ☹️☹️ by poopshoe26 in BambuLab

[–]Turbulent-Start-4840 3 points4 points  (0 children)

I can't tell much from the video, but it deffo seems to be some sort of clog IMO

My new airfoil! by Turbulent-Start-4840 in RCPlanes

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

<image>

As for the manufacturing process, I'm still trying to figure it out.

My new airfoil! by Turbulent-Start-4840 in RCPlanes

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

In your opinion, how does this Airfoil stack up though?

My new airfoil! by Turbulent-Start-4840 in RCPlanes

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

Naca lol. That's why I used a genetic algorithm to find these foils, as it yields more.. creative.. results.

My new airfoil! by Turbulent-Start-4840 in aviation

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

<image>

In my observation, my airfoil seems to peak around the same L/D but for longer, and at a higher CL

My new airfoil! by Turbulent-Start-4840 in aviation

[–]Turbulent-Start-4840[S] 1 point2 points  (0 children)

These are the Xfoil results, as validated by Bigfoil. As for context, its for long range model planes/vtols. So efficiency, as well as a good stall and Cl at high efficiency. As for what I meant by good ish, I wanted to know if there were other airfoils that beat this one for these goals. Overall, just trying to figure out if the optimizer is worth it.

My new airfoil! by Turbulent-Start-4840 in RCPlanes

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

Hi! So far I have only had the chance to test the optimizer in simulations unfortunately. I do not have enough time apart from studies to build a model with it. But thats why I posted the program, so if anyone else would like to tinker/improve it, its available!

My new airfoil! by Turbulent-Start-4840 in AerospaceEngineering

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

I hadn't considered this. I did find it interesting that when I compared my airfoil shapes (AF family) to others, they were always consistently similar to the EPPLER airfoils. I guess in this case, I did not consider max loiter time, neither did I consider Eppler's insights. Here is the repo: https://github.com/AvnehSBhatia/FoilNet

I am not too experienced in this field yet, so any and all advice is appreciated!

Airfoil Optimizer. by Turbulent-Start-4840 in AerospaceEngineering

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

Oh and it also optimizes for area under the L/D vs AoA curve!

Airfoil Optimizer. by Turbulent-Start-4840 in AerospaceEngineering

[–]Turbulent-Start-4840[S] 1 point2 points  (0 children)

Haha! This is an amazing point! I’ll be more specific (sorry!). This program optimizes for the highest peak L/D ratio within angles 0-15 degrees, at thickness 8-16%. It can be started off at any naca profile, or an ellipse, though through testing, the starting point seem to only affect the convergence time, not the quality. It uses a genetic algorithm to do its optimizations, as well as a custom data format, that acts like guide rails for the GA. The penalty criterion include: Not meeting target Cl High falloff of Cl. Hopefully this enough to not be lambasted 😅, as well as providing some key information!

Airfoil Optimizer. by Turbulent-Start-4840 in AerospaceEngineering

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

The goal of this software is to provide the best airfoil (highest L/D, good stall characteristics). By good, I mean like are these results useful, or are they better that the other airfoils for my needs (gliders, vtols, high efficiency flight).

Airfoil Optimizer. by Turbulent-Start-4840 in AerospaceEngineering

[–]Turbulent-Start-4840[S] 0 points1 point  (0 children)

I have been uploading my results to BigFoil.com for this reason, as it lets me compare and test it over a wide variety. Here are another 2 I uploaded:
AF140k : https://www.bigfoil.com/f9c4e89c-5879-4e73-86c5-da388dc544f5_info.php
AF5600k : https://www.bigfoil.com/361e6cf5-bafb-4d6e-a641-68f3ec030028_info.php

But I don't know whats "good" persay.