Excellent video. I am scratch building an rc plane that is unstable in flight probably due to the sizing of my control surfaces--will use the info in your video to correct. If you did a video on C-loading: cubic loading versus ounces per square feet, I think a lot of viewers may find that interesting. Thanks for sharing.
It would be better if you can please tell, what kind of plane or what flight characteristics are you targeting because these ratios are different for different types of planes.
Mam could please making the video on the on 3 parts of fuselage complete dimensions and calculations and also how much angle deviation at the f3 part of fuselage
This is far from anything but a wild ass guess approach. Start with analyzing an existing model that performs like you intend your design to perform. Then move ahead by fine tuning and testing.
What will be the calculation of 7inch chord length let's say wing span is 42inch plane ... You said H stabilizer is 15 to 20% of wing span someone said 20 to 25% of wing span when maintaining 3:1 aspect it's pain in the ass so please tell us what is right and what is wrong
some info. you Should be using drawings that show Correct PROPORTIONS. the (prevalent) use of Heavy materials results in Every scratch-built model being Heavy for its size (and having tail-heaviness in its dom. distribution of mass). good airframe design can be achieved, where One fundamental dimension is determined; that being, either, prop diameter or wingspan range. in this case, design priority should be given to wingspan. these heavy models need to have a wingspan of one meter/yard or greater. with this information, the other dimensions can be determined; via the use of a few Ratios/math. questions. googletranslate
see my comment. at linked drawings. note the fuselage is shaped like an elongated teardrop or top-view of a trout. at any scale, correct airframe design boils-down to RATIOS!!! at second link, a CORRECT illustration of a typical cessna high-wing design; the ideal location of c-m is indicated. center of mass. cheers upload.wikimedia.org/wikipedia/commons/thumb/6/63/Dreiseitenansicht_Cessna_172.svg/1280px-Dreiseitenansicht_Cessna_172.svg.png s3.amazonaws.com/assets.flitetest.com/article_images/medium/truecg-jpg_1384168691.jpg
One of the best videos, i will confirm these calculations, as i am building the one.
tell us vedios useful to fly a plane???
Excellent video. I am scratch building an rc plane that is unstable in flight probably due to the sizing of my control surfaces--will use the info in your video to correct. If you did a video on C-loading: cubic loading versus ounces per square feet, I think a lot of viewers may find that interesting. Thanks for sharing.
amazing stuff...thank you !!! also, loved your pleasant voice
Thank you so much😁.
Pleasant voice lol 😅
It would be better if you can please tell, what kind of plane or what flight characteristics are you targeting because these ratios are different for different types of planes.
Right, here we are targeting the trainer planes.
Great Video!
Thanks!
Which is the reference you used to do tha calculations?
Please make video on Design of aircraft by putting wing span constant
Will work on it.
Thank u
Mam could please making the video on the on 3 parts of fuselage complete dimensions and calculations and also how much angle deviation at the f3 part of fuselage
Great work mam
Thank you 😊
Nice 🤗🤗
What about taper wings ??
very helpful
what are you basing your calculations off? A real life plane that has been scaled down?
What about the thickness of the plane?
Hi, thanks for your comment. Are you referring to the thickness of the material you plan to use?
Mam I have Two questions -
1) What is Wing root chord ? and
2) Agar Wing leading age se tapered hai to iska CG calculation kaise karenge ?
This is far from anything but a wild ass guess approach. Start with analyzing an existing model that performs like you intend your design to perform. Then move ahead by fine tuning and testing.
How do you get the dimensions? Pls explain
Hi we can't see what you are writing could you put the calculation as pdf
Top 👍👍
This stuff is for specialized people and technicians
What will be the calculation of 7inch chord length let's say wing span is 42inch plane ... You said H stabilizer is 15 to 20% of wing span someone said 20 to 25% of wing span when maintaining 3:1 aspect it's pain in the ass so please tell us what is right and what is wrong
👏👏👏
Thank you
yeah Good one...
Thanks ✌️
Can u clear my doubts ??
yeah what's your doubt?
😍💯💯
Thank you
👍👍👍
thank you
some info. you Should be using drawings that show Correct PROPORTIONS. the (prevalent) use of Heavy materials results in Every scratch-built model being Heavy for its size (and having tail-heaviness in its dom. distribution of mass). good airframe design can be achieved, where One fundamental dimension is determined; that being, either, prop diameter or wingspan range. in this case, design priority should be given to wingspan. these heavy models need to have a wingspan of one meter/yard or greater. with this information, the other dimensions can be determined; via the use of a few Ratios/math. questions. googletranslate
It’s honestly more reasonable if you apply Dimensional Analysis for the scaling of your craft
help me with this stuff...difficult to understand
see my comment. at linked drawings. note the fuselage is shaped like an elongated teardrop or top-view of a trout. at any scale, correct airframe design boils-down to RATIOS!!! at second link, a CORRECT illustration of a typical cessna high-wing design; the ideal location of c-m is indicated. center of mass. cheers
upload.wikimedia.org/wikipedia/commons/thumb/6/63/Dreiseitenansicht_Cessna_172.svg/1280px-Dreiseitenansicht_Cessna_172.svg.png
s3.amazonaws.com/assets.flitetest.com/article_images/medium/truecg-jpg_1384168691.jpg
you can write your doubt here so that we can clear it or to aeronauts2920@gmail.com
if interested, see my tutorials.
🤔🤨😐😑😶🙄😛😜😝