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Impingement of Water Droplets on an Ellipsoid with Fineness Ration 10 in Axisymmetric FlowThe presence of radomes and instruments that are sensitive to water films or ice formations in the nose section of all-weather aircraft and missiles necessitates a knowledge of the droplet impingement characteristics of bodies of revolution. Because it is possible to approximate many of these bodies with an ellipsoid of revolution, droplet trajectories about an ellipsoid of revolution with a fineness ratio of 10 were computed for incompressible axisymmetric air flow. From the computed droplet trajectories, the following impingement characteristics of the ellipsoid surface were obtained and are presented in terms of dimensionless parameters: (1) total rate of water impingement, (2) extent of droplet impingement zone, and (3) local rate of water impingement. These impingement characteristics are compared briefly with those previously reported for an ellipsoid of revolution with a fineness ratio of 5.
Document ID
19930083846
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Technical Note
Authors
Brun, Rinaldo J
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Dorsch, Robert G
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
May 1, 1954
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-TN-3147
Report Number: NACA-TN-3147
Accession Number
93R13136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
METEOROLOGY
FLOW, INCOMPRESSIBLE
ICE PREVENTION AND REMOVAL
ICE FORMATION
BODIES - SURFACE CONDITIONS
MISSILES
ICE PREVENTION AND REMOVAL - ACCESSORIES, MISCELLANEOUS
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