Rocket-Powered Model Investigation of Lift, Drag, and Stability of a Body-Tail Configuration at Mach Numbers From 0.8 to 2.3 and Angles of Attack Between Plus or Minus 6.5 Degrees

Author:	Gillespie, Warren, Jr.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L54C04
Link:	https://digital.library.unt.edu/ark:/67531/metadc60300/