Turbulent boundary-layer and skin-friction measurements in axial flow along cylinders at Mach numbers between 0.5 and 3.6

Author:	Chapman, Dean R.
Year:	1954
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3097
Link:	https://digital.library.unt.edu/ark:/67531/metadc56932/