Pieliker96
Elite member
I finished and maidened the 100mm XF Viper!Using two 3300mAh 6S packs in series for insane 12S power, it flew for about 4min. It's probably hard to grasp from the pics, but that thing is HUGE! About 175cm long.
Conclusions:
In conclusion, this was definitely a fun project, but I feel like the very high-end electronics and powertrain I have on this plane would be better suited for a more sturdy plane - even after just one good flight, you can already see the maker foam looking very worn in many places. Ultimately, I think the material just doesn't scale up that well for heavy/large planes. Thus, I'll probably take out the electronics and build something else. Still, many thanks to Ben for the excellent plans! I will most likely build another, but at its original size.
- Hand launching it is difficult (but doable once you find the right technique)... Unfortunately I scrunched the nose on the first attempt, but that didn't stop me from trying again.
- It feels like the EDF is not getting enough air, making it less powerful than it could be... unfortunate, but that's just due to the F-16's design.
- It's not extremely fast, but not exactly slow either.
- The maximum roll rate, as predicted by Ben, is insane!
- Belly-landing is no problem, even at >4kg AUW.
- The batteries get VERY hot, due to having no airflow over them - this would really hurt them in the long term.
- The carbon fiber reinforcements I made were definitely necessary!
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One thing you may want to check with regards to performance is your nozzle exit diameter and area. Compare that to the Fan-Swept Area (FSA) - the area of the fan's frontal area minus the area of the motor and hub. From this post it doesn't visually look like there's any taper to the thrust tube, which is required to get the exit area equal to or smaller than the FSA (≤100%). A straight pipe with no taper will be at over 100% FSA which will lose both static (stationary) and dynamic (in-flight) thrust. 100% FSA optimizes for static thrust, and more constricted means higher top speed with the tradeoff of lower thrust at lower speeds - 90% is a good starting point. Constricting the nozzle exit area if it is indeed over 100% has the potential to drastically improve performance.