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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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