Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method

Author:	Lina, Lindsay J.
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L9A12
Link:	https://digital.library.unt.edu/ark:/67531/metadc58214/