Investigation of a triangular wing in conjunction with a fuselage and horizontal tail to determine downwash and longitudinal-stability characteristics: transonic bump method

Author:	Allen, Edwin C.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A51F12a
Link:	https://digital.library.unt.edu/ark:/67531/metadc59054/