Measurements of the effects of finite span on the pressure distribution over double-wedge wings at Mach numbers near shock attachment

Author:	Vincenti, Walter G
Year:	1955
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3522
Link:	https://digital.library.unt.edu/ark:/67531/metadc57614/