The Effect of Wing Profile on the Transonic Characteristics of Rectangular and Triangular Wings Having Aspect Ratios of 3: Transonic Bump Technique

Author:	Nelson, Warren H.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A54H12a
Link:	https://digital.library.unt.edu/ark:/67531/metadc60973/