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A flight investigation of the boundary-layer characteristics and profile drag of the NACA 35-215 laminar-flow airfoil at high Reynolds numbers
Author:
Platt, Robert C.
Year:
1941
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-532, NACA-MR
Link:
https://digital.library.unt.edu/ark:/67531/metadc61113/
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