skip to content
Effects of angle of attack and airfoil profile on the two-dimensional flutter derivatives for airfoils oscillating in pitch at high subsonic speeds
Author:
Wyss, John A.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A54H12
Link:
https://digital.library.unt.edu/ark:/67531/metadc60982/
< New search