Effect of variation of chord and span of ailerons on rolling and yawing moments at several angles of pitch

Author:	Heald, R. H.
Additional Authors:	Strother, D. H.
Year:	1929
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-343
Link:	https://digital.library.unt.edu/ark:/67531/metadc65996/