Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle

Author:	Kuhn, Richard E
Year:	1956
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3692
Link:	https://digital.library.unt.edu/ark:/67531/metadc55950/