Subsonic wind-tunnel investigation of the effect of fuselage afterbody on directional stability of wing-fuselage combinations at high angles of attack

Author:	Polhamus, Edward C.
Year:	1956
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3896
Link:	https://digital.library.unt.edu/ark:/67531/metadc56446/