A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50

Author:	Falanga, Ralph A.
Year:	1955
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L55F09A
Series:	NACA research memorandum ;
Report Number:	L55F09A
Subjects:	Charts, diagrams, etc
	Drag (Aerodynamics)
	Jets--Fluid dynamics
Link:	https://hdl.handle.net/2027/mdp.39015086465898