Consider a flying-wing aircraft made using a NACA 2412

in /by

Consider a flying-wing aircraft made using a NACA 2412

Consider a flying-wing aircraft made using a NACA 2412 airfoil with a wing area of 250 ft ^2, a wing span of 50 ft, and a span efficiency factor of 0.9. If the aircraft is flying at a 6 deg angle of attack and a Reynolds number of approximately 9×10^6, what are CL and CD for the flying wing?

"You need a similar assignment done from scratch? Our qualified writers will help you with a guaranteed AI-free & plagiarism-free A+ quality paper, Confidentiality, Timely delivery & Livechat/phone Support.


Discount Code: CIPD30



Click ORDER NOW..

order custom paper