The Results of Wind-Tunnel Tests at Low Speeds 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: Buell, Donald A.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A53I28
Link: https://digital.library.unt.edu/ark:/67531/metadc59893/

< New search