The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. III : effects of trailing-edge flaps

Author:	Tinling, Bruce E.
Year:	1957
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4043
Link:	https://digital.library.unt.edu/ark:/67531/metadc56491/