Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel

Author: Campbell, John P.
Year: 1945
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-50, NACA-ACR-L5A13
Link: https://digital.library.unt.edu/ark:/67531/metadc60992/

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