Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42

Author:	Schulderfrei, Marvin
Additional Authors:	Comisarow, Paul
Year:	1951
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2482
Link:	https://digital.library.unt.edu/ark:/67531/metadc55718/