Analysis of Wind-Tunnel Tests at Low Speeds of a Four-Engine Propeller-Driven Airplane Configuration Having a Wing With 40 Degrees of Sweepback

Author: Edwards, George G.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A54F14
Link: https://digital.library.unt.edu/ark:/67531/metadc60430/

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