Some effects of aileron span, aileron chord, and wing twist on rolling effectiveness as determined by rocket-powered model tests and theoretical estimates

Author:	Strass, H. Kurt
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L54G13
Link:	https://digital.library.unt.edu/ark:/67531/metadc60614/