Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine

Author:	Czarnecki, K. R.
Year:	1946
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1087
Link:	https://digital.library.unt.edu/ark:/67531/metadc54857/