A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body

Author:	Palmer, William E.
Additional Authors:	Burrows, Dale L.
Year:	1955
Document Type:	MAIN
SUDOC:	Y 3.N21/5:15/L55A07a
Series:	NACA research memorandum ;
Report Number:	L55A07a
Subjects:	Stability of airplanes, Longitudinal
	Delta wing airplanes--Handling characteristics
Link:	https://hdl.handle.net/2027/mdp.39015095100866