Determining the Velocity Distribution in the Boundary Layer of an Airfoil Fitted With a Rotary Cylinder

Author:	Van der Hegge Zijnen, B. G.
Year:	1927
Document Type:	N/A
Series:	NACA Technical Memorandums
Report Number:	NACA-TM-411
Link:	https://digital.library.unt.edu/ark:/67531/metadc277428/