Doc. no. ZB-001 Rev. 5.0

Zhangir Begim

About:

I am a Mechanical Engineering student at The Hong Kong Polytechnic University. My interests include automotive and aerospace engineering.

Contact:

Email
zhanrocks@gmail.com
Instagram
@zhangiraeroclub
YouTube
@zhanrocks
c = 1.000 LEADING EDGE MAX. THICKNESS t = 0.12c AT 0.30c MEAN CAMBER LINE, 0.02c AT 0.40c TRAILING EDGE CHORD
Fig. 1 — NACA 2412 airfoil section

Important posts:

SectionNameDate
— No posts yet. —