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Impingement of Water Droplets on NACA 65A004 Airfoil at 8 deg Angle of AttackThe trajectories of droplets in the air flowing past an NACA 65AO04 airfoil at an angle of attack of 8 deg were determined.. The amount of water in droplet form impinging on the airfoil, the area of droplet impingement, and the rate of droplet impingement per unit area on the airfoil surface were calculated from the trajectories and presented to cover a large range of flight and atmospheric conditions. These impingement characteristics are compared briefly with those previously reported for the same airfoil at an angle of attack of 4 deg.
Document ID
19810068691
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Brun, R. J. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Gallagher, H. M. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Vogt, D. E. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
July 1, 1954
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NACA-TN-3155
Accession Number
81N73113
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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