Analysis of Wind-Tunnel Tests to a Mach Number of 0.90 of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback and an Aspect Ratio of 10

Author:	Edwards, George G.
Additional Authors:	Demele, Fred A., Buell, Donald A.
Year:	1956
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3790
Link:	https://digital.library.unt.edu/ark:/67531/metadc56014/