The results 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:	Sutton, Fred B., Dickson, Jerald K.
Year:	1956
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3789
Link:	https://digital.library.unt.edu/ark:/67531/metadc56062/