Wind-Tunnel Investigation at a Mach Number of 2.01 of Forebody Strakes for Improving Directional Stability of Supersonic Aircraft

Author:	Driver, Cornelius
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L58C11
Link:	https://digital.library.unt.edu/ark:/67531/metadc64072/