Rocket-Model Investigation to Determine the Force and Hinge-Moment Characteristics of a Half-Delta Tip Control on a 59 Degree Sweptback Delta Wing Between Mach Numbers of 0.55 and 1.43

Author:	Martz, C. William
Additional Authors:	Church, James D.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L52H06
Link:	https://digital.library.unt.edu/ark:/67531/metadc59366/