Boundary-layer transition at high Reynolds numbers as obtained in flight of a 20 degree cone-cylinder with wall to local stream temperature ratios near 1.0

Author:	Rabb, Leaonard
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55I15
Link:	https://digital.library.unt.edu/ark:/67531/metadc61627/