Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing

Author:	Polhamus, Edward C.
Additional Authors:	Spreemann, Kenneth P.
Year:	1958
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5;15/L57K15A
Series:	NACA research memorandum ;
Report Number:	L57K15A
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Airplanes--Fuselage
	Airplanes--Tail surfaces
	Airplanes--Wings, Triangular
	Airplanes--Models--Testing
	Stability of airplanes, Longitudinal
	Loads (Mechanics)
	Stability of airplanes, Lateral
Link:	https://hdl.handle.net/2027/mdp.39015086466276