Comparison of flutter calculations using various aerodynamic coefficients with experimental results for some rectangular cantilever wings at Mach number 1.3

Author:	Nelson, Herbert C.
Year:	1954
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3301
Link:	https://digital.library.unt.edu/ark:/67531/metadc57296/