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