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Impingement of Water Droplets on an NACA 65(sub 1) -212 Airfoil at an Angle of Attack of 4 DegThe trajectories of droplets in the air flowing past an NACA 651-212 airfoil at an angle of attack of 40 were determined. The collection efficiency, the area of droplet impingement, and the rate of droplet impingement were calculated from the trajectories and are presented herein.
Document ID
19810068679
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Brun, Rinaldo J. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Serafini, John S. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Moshos, George J. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
September 10, 1952
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NACA-RM-E52B12
Accession Number
81N73101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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