The effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel

Author:	Hollingworth, Thomas A
Year:	1943
Document Type:	N/A
Series:	NACA Wartime Reports
Report Number:	NACA-WR-L-220, NACA-ACR
Link:	https://digital.library.unt.edu/ark:/67531/metadc61007/