Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section

Author:	Johnson, Harold S.
Year:	1953
Document Type:	MAIN
SUDOC:	Y 3.N21/5:15/L53J05a
Series:	NACA research memorandum ;
Report Number:	L53J05a
Subjects:	Airplanes--Wings, Swept-back
	Stability of airplanes, Lateral
Link:	https://hdl.handle.net/2027/mdp.39015095100718