The interaction of boundary layer and compression shock and its effect upon airfoil pressure distributions

Author:	Allen, H. Julian
Additional Authors:	Heaslet, Max A.
Year:	1947
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A7A02
Link:	https://digital.library.unt.edu/ark:/67531/metadc57995/