Rocket-Model Investigation to Determine the Lift and Pitching Effectiveness of Small Pulse Rockets Exhausted From the Fuselage Over the Surface of an Adjacent Wing at Mach Numbers From 0.9 to 1.8

Author:	Martz, C. William
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L58G29
Link:	https://digital.library.unt.edu/ark:/67531/metadc64417/