DAE-11 AIRFOIL (dae11-il) Xfoil prediction polar at RE=50,000 Ncrit=5
DAE-11 AIRFOIL (dae11-il) Xfoil prediction polar at RE=50,000 Ncrit=5 Airfoil Tools Search 1638 airfoils Tweet You have 0 airfoils loaded. Your Reynold number range is 50,000 to 1,000,000.
Polar details for airfoil (aerofoil)DAE-11 AIRFOIL(dae11-il) Xfoil prediction at Reynolds number 50,000 and Ncrit 5