Can you please explain the types of air foils used in aircrafts with their properties
@nevillecreativitymentorАй бұрын
I cannot find any details on the FREE Subscription .. I want to try it out first.
@pulsarspacetimeАй бұрын
Absolutely interesting video and very broken down!! 👏👏
@ginonguegang9232Ай бұрын
The correct lift equation has the aircraft wing area and not the wing chord
@CarlosChavez-gs1ld2 ай бұрын
Buen Hecho Juan. Gracias.
@pjdava2 ай бұрын
SIMNET, I love your channel so much, I just had to subscribe!
@jamcof2 ай бұрын
Great video!
@Boogie3D2 ай бұрын
2:25 You should specify it better. From your description you can have a relatively thin (5-6%) undercambered airfoil and the max difference betwwen upper and lower surface would make it something like 7-8%.
@FrontSideBus2 ай бұрын
Don't you mean an aerofoil?
@mubasshir2 ай бұрын
American English
@JohanFasth2 ай бұрын
But that is not how lift is generated. It is much more complicated than that. Here is the correct explanation. kzread.info/dash/bejne/g393rZaleq-3eLg.html
@hetavparikh94882 ай бұрын
Very useful and knowlwdgable video I must say. I was researching the resources to fairly design the airfoil and came across your video series. It cleared quite few questions for me. Thanks a lot for making this video seires and will be waiting for new videos. 🙌
@FPVREVIEWS3 ай бұрын
The video touched on the subject but didn’t actually talk about it. That’s the forward shift in CP with increase of AOA. Dealing with the effects of camber on the pitch of the aircraft, maintaining stability without losing efficiency is a major design challenge and something for consideration when choosing the overall aircraft configuration. It’s actually possible to achieve aerodynamic instability with dynamic stability at the same time with no moving parts.
@davidg39443 ай бұрын
Thanks, this is a well-presented video. Looking forward to whatever else you produce on the subject of low-speed aerodynamics.
@bartekprzybylski11693 ай бұрын
Very good video! I like it a lot. Can i make a suggestion to change colour of airfoil and graphs for brighter for better visibility of diffrences :-) Good luck with Your project!
@SIMNET_aero3 ай бұрын
Thanks for your comment and suggestion, we'll improve the image contrast for part 2 of the series.
@MTFTVlive3 ай бұрын
Easily the most comprehensive video on the intenet. I've been searching for something like this for weeks, imagine my surprise seeing this video was only a day old. Subscribed!
@SIMNET_aero3 ай бұрын
Thanks for the feedback! Stay tuned for part 2 which will offer many practical tips and tricks for airfoil selection. If you have any other topics you would like us to cover, feel free to let us know.
@MTFTVlive3 ай бұрын
@@SIMNET_aero yeah I’d love to see differences between pusher and puller prop configurations aerodynamically, I’m currently trying to build a 3d printed fixed wing drone using the inrunners from an junked $20 quad
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Can you please explain the types of air foils used in aircrafts with their properties
I cannot find any details on the FREE Subscription .. I want to try it out first.
Absolutely interesting video and very broken down!! 👏👏
The correct lift equation has the aircraft wing area and not the wing chord
Buen Hecho Juan. Gracias.
SIMNET, I love your channel so much, I just had to subscribe!
Great video!
2:25 You should specify it better. From your description you can have a relatively thin (5-6%) undercambered airfoil and the max difference betwwen upper and lower surface would make it something like 7-8%.
Don't you mean an aerofoil?
American English
But that is not how lift is generated. It is much more complicated than that. Here is the correct explanation. kzread.info/dash/bejne/g393rZaleq-3eLg.html
Very useful and knowlwdgable video I must say. I was researching the resources to fairly design the airfoil and came across your video series. It cleared quite few questions for me. Thanks a lot for making this video seires and will be waiting for new videos. 🙌
The video touched on the subject but didn’t actually talk about it. That’s the forward shift in CP with increase of AOA. Dealing with the effects of camber on the pitch of the aircraft, maintaining stability without losing efficiency is a major design challenge and something for consideration when choosing the overall aircraft configuration. It’s actually possible to achieve aerodynamic instability with dynamic stability at the same time with no moving parts.
Thanks, this is a well-presented video. Looking forward to whatever else you produce on the subject of low-speed aerodynamics.
Very good video! I like it a lot. Can i make a suggestion to change colour of airfoil and graphs for brighter for better visibility of diffrences :-) Good luck with Your project!
Thanks for your comment and suggestion, we'll improve the image contrast for part 2 of the series.
Easily the most comprehensive video on the intenet. I've been searching for something like this for weeks, imagine my surprise seeing this video was only a day old. Subscribed!
Thanks for the feedback! Stay tuned for part 2 which will offer many practical tips and tricks for airfoil selection. If you have any other topics you would like us to cover, feel free to let us know.
@@SIMNET_aero yeah I’d love to see differences between pusher and puller prop configurations aerodynamically, I’m currently trying to build a 3d printed fixed wing drone using the inrunners from an junked $20 quad
Amazing! Well explained
Thank you for sharing.
This is super cool
Waooo
Thank you for info been searching for right one