Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01

Author:	Spearman, M. Leroy.
Additional Authors:	Robinson, Ross B.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L57J25A
Series:	NACA research memorandum ;
Report Number:	L57J25A
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Mach number
	Pitching (Aerodynamics)
	Airplanes--Wings, Swept-back
	Airplanes--Tail surfaces
	Stability of airplanes, Lateral
Link:	https://hdl.handle.net/2027/mdp.39015086466235