Mac790
Well-Known Member
This time I have a more serious problem, I have to make a J-1B DON QUIXOTE model for a flow analysis (another uni project), and I can't find coordinates for the clarkY 13% airfoil, I've found coordintes for a normal Clark Y(attachment), and I'm familiar with this page
UIUC Airfoil Coordinates Database
Does anyone know when I can find it or how to "transfer/change" normal foil into 13% thick one (multiply +,- coordinates by 13%?), sorry for silly question but I'm studing mechanical not aeronautical engineering and I'm not extremely familiar with this..
Seb
UIUC Airfoil Coordinates Database
Does anyone know when I can find it or how to "transfer/change" normal foil into 13% thick one (multiply +,- coordinates by 13%?), sorry for silly question but I'm studing mechanical not aeronautical engineering and I'm not extremely familiar with this..
Seb