Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60©� delta wing and a high unwept horizontal tail

Author:	Peck, Robert F.
Additional Authors:	Mitchell, Jesse L.
Year:	1953
Document Type:	MAIN
SUDOC:	Y 3.N 21/5:15/L52K04a
Series:	NACA research memorandum ;
Report Number:	L52K04a
Subjects:	Stability of airplanes, Longitudinal
	Delta wing airplanes
Link:	https://hdl.handle.net/2027/mdp.39015095100668