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Aerodynamic Tests of an NACA 66(215)-116, a=0.6 Airfoil With a 0.25c Slotted Flap for the Fleetwings XA-39 Airplane
Author:
Cahill, Jones F.
Year:
1944
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-629, NACA-MR-L4K21
Link:
https://digital.library.unt.edu/ark:/67531/metadc61411/
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