Preliminary results of the flight investigation between Mach numbers of 0.80 and 1.36 of a rocket-powered model of a supersonic airplane configuration having a tapered wing with circular-arc sections and 40©� sweepback

Author:	D'Aiutolo, Charles T.
Additional Authors:	Mason, Homer P.
Year:	1958
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L50H29a
Series:	NACA research memorandum ;
Report Number:	L50H29a
Subjects:	Supersonic planes
	Yawing (Aerodynamics)--Testing
	Stability of airplanes, Longitudinal--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086464693