Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region

Author:	Pierce, Harold B.
Additional Authors:	Reisert, Thomas D.
Year:	1955
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L55H22B
Series:	NACA research memorandum ;
Report Number:	L55H22B
Subjects:	Charts, diagrams, etc
	Aerodynamic load
	Wind tunnel testing
	Airplanes--Models--Testing
	Airplanes--Models--Wings
	Gust loads
Link:	https://hdl.handle.net/2027/mdp.39015086465948