Your videos are so great sir! Im doing some cfd for f1 wings, and Im facing some troubles I have a 3 elements wing, but I don't know how to calculate the planform area Should I adjust all the 3 elements to zero AoA, then taking the planform area? Or should I consider all the 3 elements as 1 indivisual wing and then taking the planform area? And if I did the second choice, should the equvalent wing be in zero AoA or what?? Please let me know
Im struggling with planform area of multi elemnts wing Im very confused!! I don't know what chord line to use and what are the conditions to be achieved for this chord line
Scaling factor for these airfoils are similar to aspect ratio of a 2D image. Usually when you look at literature where there are multiple airfoil elements, the designer specifies what percent of the chord is the high-lift device (HLD), or what percentage of chord is the main airfoil.
Had to come to see this again. Will be working on it tomorrow! :)
Your videos are so great sir!
Im doing some cfd for f1 wings, and Im facing some troubles
I have a 3 elements wing, but I don't know how to calculate the planform area
Should I adjust all the 3 elements to zero AoA, then taking the planform area?
Or should I consider all the 3 elements as 1 indivisual wing and then taking the planform area?
And if I did the second choice, should the equvalent wing be in zero AoA or what??
Please let me know
Im struggling with planform area of multi elemnts wing
Im very confused!!
I don't know what chord line to use and what are the conditions to be achieved for this chord line
Sos un capo 👍
I use javafoil in a simulation but i don't understand something , can you help me
very helpfull!!
Bro can you tell me a bit about scaling factor?
Scaling factor for these airfoils are similar to aspect ratio of a 2D image. Usually when you look at literature where there are multiple airfoil elements, the designer specifies what percent of the chord is the high-lift device (HLD), or what percentage of chord is the main airfoil.
is there java foil for mac?
I believe there is JavaFoil version that runs on Mac, but I have never tried it. You have to find it yourself. Sorry.
I am not getting it's dat file..can you please mail me?
dat file for the NACA 23012 airfoil OR data for experimental validation ?
@@coolkid2329094 sir, kindly give your e-mail address, I want to contact you.
Comment je peux telechrger java foil est-ce qu’il est gratuit
Hi Ayoub, yes JavaFoil is a free program. You download it from the website of mh-aerotools.de/airfoils/
Why did you put the song ahahahah
Otherwise, javafoil tool will not work 🤣
@@coolkid2329094 ahhh issue solved, thanks😂
How to download javafoil on pc?
www.mh-aerotools.de/airfoils/javafoil.htm
It has been a while since I worked with JavaFoil, but this link should be sufficient.