Obtain the quasi unsteady lift coefficient using FFT and the arbitrary angle of attack change associated with
Question:
Obtain the quasi unsteady lift coefficient using FFT and the arbitrary angle of attack change associated with the equivalent quasi steady lift given by Eq. 8.51 for the reduced frequency of 0.8 and 1.0 . Comment on the differences of both lift coefficient curves.
Eq. 8.51
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: