Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-Foot-Span Fighter-Type Wing of NACA 230-Series Airfoil Sections

Author:	Pearson, E. O., Jr.
Additional Authors:	Evans, A. J.
Year:	1945
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-L-51, NACA-ACR-L5G10
Link:	https://digital.library.unt.edu/ark:/67531/metadc61423/