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Impingement of Water Droplets on NACA 65A004 Airfoil and Effect of Change in Airfoil Thickness from 12 to 4 Percent at 4 deg Angle of Attack
Author:
Brun, Rinaldo J.
Additional Authors:
Gallagher, Helen M.
Year:
1953
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3047
Link:
https://digital.library.unt.edu/ark:/67531/metadc53479/
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