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Particle trajectory computation on a 3-dimensional engine inletA 3-dimensional particle trajectory computer code was developed to compute the distribution of water droplet impingement efficiency on a 3-dimensional engine inlet. The computed results provide the essential droplet impingement data required for the engine inlet anti-icing system design and analysis. The droplet trajectories are obtained by solving the trajectory equation using the fourth order Runge-Kutta and Adams predictor-corrector schemes. A compressible 3-D full potential flow code is employed to obtain a cylindrical grid definition of the flowfield on and about the engine inlet. The inlet surface is defined mathematically through a system of bi-cubic parametric patches in order to compute the droplet impingement points accurately. Analysis results of the 3-D trajectory code obtained for an axisymmetric droplet impingement problem are in good agreement with NACA experimental data. Experimental data are not yet available for the engine inlet impingement problem analyzed. Applicability of the method to solid particle impingement problems, such as engine sand ingestion, is also demonstrated.
Document ID
19860010908
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Kim, J. J.
(Wichita State Univ. Wichita, KS, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Air Transportation And Safety
Report/Patent Number
DOT-FAA-CT-86-1
NASA-CR-175023
NAS 1.26:175023
Report Number: DOT-FAA-CT-86-1
Report Number: NASA-CR-175023
Report Number: NAS 1.26:175023
Accession Number
86N20379
Funding Number(s)
PROJECT: RTOP 505-68-11
CONTRACT_GRANT: NAG3-566
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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