×
+ All Categories
Log in
English
Français
Español
Deutsch
Report -
LIFT, DRAG AND MOMENT OF A NACA 0015 AIRFOILsmiller.sbyers.com/temp/AE510_03 NACA 0015 Airfoil.pdf · ABSTRACT A NACA 0015 symmetrical airfoil with a 15% thickness to chord ratio
Name
Email
Select
Select
Pornographic
Defamatory
Illegal/Unlawful
Spam
Other Terms Of Service Violation
File a copyright complaint
Message
Please pass captcha verification before submit form