Static longitudinal and lateral stability and control characteristics of an airplane configuration having a wing of trapezoidal plan form with various tail airfoil sections and tail arrangements at a Mach number of 6.86

Author:	Penland, Jim A
Additional Authors:	Fetterman, David E , Jr
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55F17
Link:	https://digital.library.unt.edu/ark:/67531/metadc61512/