Experimental determination of the aerodynamic derivatives arising from acceleration in sideslip for a triangular, a swept, and an unswept wing

Author:	Riley, Donald R
Additional Authors:	Bird, John D
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55A07
Link:	https://digital.library.unt.edu/ark:/67531/metadc61187/