Kim, J. J. (1986). Particle Trajectory Computation on a 3-Dimensional Engine Inlet (Report No. NASA Contractor Report 175023, DOT-FAA-CT-86-1). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/92637
Kim, John J.. Particle Trajectory Computation on a 3-Dimensional Engine Inlet. Report no. NASA Contractor Report 175023, DOT-FAA-CT-86-1. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1986. https://rosap.ntl.bts.gov/view/dot/92637.
Kim, John J. Particle Trajectory Computation on a 3-Dimensional Engine Inlet. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1986, Report no. NASA Contractor Report 175023, DOT-FAA-CT-86-1, ROSA P. https://rosap.ntl.bts.gov/view/dot/92637.
A 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 flow field 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.
Kim, J. J. (1986). Particle Trajectory Computation on a 3-Dimensional Engine Inlet (Report No. NASA Contractor Report 175023, DOT-FAA-CT-86-1). United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center. https://rosap.ntl.bts.gov/view/dot/92637
Kim, John J.. Particle Trajectory Computation on a 3-Dimensional Engine Inlet. Report no. NASA Contractor Report 175023, DOT-FAA-CT-86-1. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1986. https://rosap.ntl.bts.gov/view/dot/92637.
Kim, John J. Particle Trajectory Computation on a 3-Dimensional Engine Inlet. United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center, 1986, Report no. NASA Contractor Report 175023, DOT-FAA-CT-86-1, ROSA P. https://rosap.ntl.bts.gov/view/dot/92637.
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