Pressure distributions on triangular and rectangular wings to high angles of attack Mach numbers 1.45 and 1.97

Author:	Kaattari, George E.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A54D19
Link:	https://digital.library.unt.edu/ark:/67531/metadc60492/