Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data

Author:	Martina, Albert P.
Year:	1953
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1167
Link:	https://digital.library.unt.edu/ark:/67531/metadc60546/