Wind-Tunnel Investigation of a Ram-Jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form With 70 Degree Swept Leading Edges: Force and Moment Characteristics of Various Combinations of Components at a Mach Number of 1.6

Author:	Hamilton, Clyde V.
Additional Authors:	Driver, Cornelius
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53A14
Link:	https://digital.library.unt.edu/ark:/67531/metadc59538/