An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel

Author:	McLellan, Charles H.
Additional Authors:	Bertram, Mitchel H.
Year:	1951
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1310
Link:	https://digital.library.unt.edu/ark:/67531/metadc60707/