Analysis method for inertial particle separator

Farooq Saeed*, Ahmad Z. Al-Garni

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

52 Scopus citations

Abstract

This paper describes an analysis method for an inertial particle separator system modeled as a multi-element airfoil configuration. The analysis method is implemented in a numerical tool that is able to perform impingement analysis using spherical, nonspherical particles as well as water droplets for a range of Reynolds number (10-4 ≤ Re ≤ 5 × 105). A limitations of the analysis tool is that it lacks an appropriate particle rebound model for the treatment of particle-wall collisions. The usefulness of the analysis tool is its use in conjunction with a multipoint inverse design tool for the design of a multi-element airfoil based inertial particle separator system model in an inverse fashion as opposed to the direct design methods being employed currently for this task. With such a design and analysis tool at hand, the design space can be explored as well as tradeoff studies can be performed that can aid in the development of a more efficient design methodology for multi-element airfoil based inertial particle separator systems.

Original languageEnglish
Pages (from-to)1150-1158
Number of pages9
JournalJournal of Aircraft
Volume44
Issue number4
DOIs
StatePublished - 2007

ASJC Scopus subject areas

  • Aerospace Engineering

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