Transonic wind-tunnel investigation of aerodynamic-loading characteristics of a 2-percent-thick trapezoidal wing in combination with basic and indented bodies

Author:	Kelly, Thomas C.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56J12a
Series:	NACA research memorandum ;
Report Number:	L56J12a
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Airplanes--Fuselage
	Aerodynamic load--Measurement
	Airplanes--Wings, Trapezoidal
Link:	https://hdl.handle.net/2027/mdp.39015086507152