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Impingement of Droplets in 90 deg Elbows with Potential FlowTrajectories were determined for droplets in air flowing through 90 deg elbows especially designed for two-dimensional potential motion with low pressure losses. The elbows were established by selecting as walls of each elbow two streamlines of the flow field produced by a complex potential function that establishes a two-dimensional flow around a 90 deg bend. An unlimited number of elbows with slightly different shapes can be established by selecting different pairs of streamlines as walls. The elbows produced by the complex potential function selected are suitable for use in aircraft air-intake ducts. The droplet impingement data derived from the trajectories are presented along with equations in such a manner that the collection efficiency, the area, the rate, and the distribution of droplet impingement can be determined for any elbow defined by any pair of streamlines within a portion of the flow field established by the complex potential function. Coordinates for some typical streamlines of the flow field and velocity components for several points along these streamlines are presented in tabular form.
Document ID
19810068680
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Hacker, Paul T.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Brun, Rinaldo J.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Boyd, Bemrose
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
September 1, 1953
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NACA-TN-2999
Report Number: NACA-TN-2999
Accession Number
81N73102
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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