skip to content
Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6
Author:
Unangst, John R.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55I13a
Link:
https://digital.library.unt.edu/ark:/67531/metadc61634/
< New search