A numerical investigation of droplet/particle impingement on a dynamic airfoil

Christian M. Sarofeen, Michael P. Kinzel, Ralph W. Noack, Richard E. Kreeger

Research output: Chapter in Book/Report/Conference proceedingConference contribution

7 Scopus citations

Abstract

In this paper we investigate phenomena associated with particle impingement on dynamic airfoils. Using an Eulerian based solver, a droplet velocity field is computed throughout the computational domain. This solver is used to scrutinize particular concepts, with the intent to save computation time, listed as follows: (i) The applicability of different time-averaging techniques to calculate an average local collection efficiency for dynamic simulations. (ii) Comparison between static and dynamic bodies undergoing particle surface interactions. (iii) The use of a numerically viscous solution to the Euler equations instead of a fully viscous solution to predict proper particle trajectories on dynamic airfoils. Guidance is provided herein, for the applicability of solution methods to reduce computational costs.

Original languageEnglish (US)
Title of host publication28th AIAA Applied Aerodynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781617389269
DOIs
StatePublished - 2010

Publication series

Name28th AIAA Applied Aerodynamics Conference
Volume1

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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