Search found 1379 matches
- Tue Feb 16, 2021 1:22 pm
- Forum: Unrelated Nonsense
- Topic: A point to learn
- Replies: 1
- Views: 18367
- Tue Feb 16, 2021 12:14 pm
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
https://forum.flightgear.org/viewtopic.php?f=17&t=38762 I think this is an interesting topic, especially for helicopters, where glancing at the gauges repeatedly is needed, and you don't really want to move the view cause a lots happening. I think I'd like a single key press to call this up and ...
- Tue Feb 16, 2021 11:20 am
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
Yes that would make sense, but it''s effect on the main rotor rpm's should be minimal. There is however rpm variations of the main rotor caused by it's governor 'hunting' the rpm's around the 324 value. My code used this value to govern the tail rotor rpm, which because of the increase in rpm's of t...
- Tue Feb 16, 2021 9:19 am
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
A lot of spanners got thrown into the machinery it's taking time to understand all the implications. And my understanding changes on a daily basis... Yesterday I thought the RPM of the tail rotor shaft was for torque, but after last nights work my thoughts are it's actually to ensure the rpm's of th...
- Mon Feb 15, 2021 9:26 am
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
Ok located that info here https://www.quora.com/How-does-a-helicopter-piston-engine-rotate-the-rotor-head 3 support bearings and 2 bevel gearboxes also given me speed of tail rotor rpm. [edit] oh wow I just found out the tail drive shaft is at 40,863 RPM... with the two bevel gearboxes reducing this...
- Sun Feb 14, 2021 11:25 am
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
Next question, you might be able to answer.
Typically how many universal joints in the tail rotor drive-chain.
I'm trying to work out it's efficiency.
So far I have this
gear box efficiency = 0.941
3 universal joints at 0.99
Angular take-off efficiency = 0.931
regards
Simon
Typically how many universal joints in the tail rotor drive-chain.
I'm trying to work out it's efficiency.
So far I have this
gear box efficiency = 0.941
3 universal joints at 0.99
Angular take-off efficiency = 0.931
regards
Simon
- Sat Feb 13, 2021 4:50 pm
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
ok no worries.... I think I'm going to have to enable some auto rudder control for twisties, otherwise I won't even be able to test it.
- Sat Feb 13, 2021 10:59 am
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
Another question on your set up. Is your joystick capable of being a twisty ? If so could you do me the favour of disconnecting your peddles and flying all the different types of helicopter flight models, not just mine. I'd like you to do this, if you can so as you have a clear understanding of the ...
- Sat Feb 13, 2021 9:10 am
- Forum: Aircraft Development
- Topic: Bell UH-1
- Replies: 218
- Views: 131291
Re: Bell UH-1
high rightside crosswind I would have assumed high leftside crosswind with vortex ringstate setting in on the tail rotor [edit]... yes high rightside crosswind will effect the advance ratio of the tail rotor prop reducing it's effectiveness. So I suspect both exist and maybe the right side is more ...
- Sat Feb 13, 2021 8:53 am
- Forum: Aircraft Development
- Topic: Avatar Scorpion
- Replies: 131
- Views: 76087
Re: Avatar Scorpion
One of the issues with using 3d models is their accuracy, they're not engineering quality they're game quality.
Also they're not solid models they're surface models and I'm not sure if a surface can be converted into a solid model, normally it's done the other way.
Also they're not solid models they're surface models and I'm not sure if a surface can be converted into a solid model, normally it's done the other way.