Pressure Distribution Tests on PW-9 Wing Models From -18 Degree Through 90 Degree Angle of Attack

Author:	Loeser, Oscar E., Jr.
Year:	1928
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-296
Link:	https://digital.library.unt.edu/ark:/67531/metadc65950/