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 language | English |
|---|---|
| Pages (from-to) | 1150-1158 |
| Number of pages | 9 |
| Journal | Journal of Aircraft |
| Volume | 44 |
| Issue number | 4 |
| DOIs | |
| State | Published - 2007 |
ASJC Scopus subject areas
- Aerospace Engineering