Free spinning wind-tunnel tests of a low-wing monoplane with systematic wings and tails 2: Mass distributed along the fuselage

Author:	Seidman, Oscar
Year:	1937
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-630
Link:	https://digital.library.unt.edu/ark:/67531/metadc54437/