An airfoil is given by a parabolic camber line, i.e., (z_{a}=-left(a / b^{2} ight) x^{2}). Find: (i)
Question:
An airfoil is given by a parabolic camber line, i.e., \(z_{a}=-\left(a / b^{2}\right) x^{2}\). Find:
(i) sectional lift coefficient,
(ii) center of pressure,
(iii) aerodynamic center, at zero angle of attack.
Fantastic news! We've Found the answer you've been seeking!
Step by Step Answer:
Related Book For
Fundamentals Of Modern Unsteady Aerodynamics
ISBN: 9783030607760,9783030607777
3rd Edition
Authors: Ülgen Gülçat
Question Posted: