Static stability and control characteristics of a triangular wing and canard configuration at Mach numbers form 2.58 to 3.53

Author:	Hedstrom, C. Ernest
Additional Authors:	Blackaby, James R.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A58C05
Link:	https://digital.library.unt.edu/ark:/67531/metadc64052/