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Preliminary Aerodynamic Investigation of the Effect of Camber on a 60 Degree Delta Wing with Round and Beveled Leading Edges
Author:
Riebe, John M.
Year:
1949
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9F10
Link:
https://digital.library.unt.edu/ark:/67531/metadc58390/
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