(2007) An Analysis Method for Inertial Particle Separator. AIAA Journal of Aircraft, 44 (4). pp. 1150-1158.
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PDF (IPS Analysis Journal Paper)
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Abstract
The paper describes an analysis method for an inertial particle separator (IPS) 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, non-spherical 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 multi-element airfoil based IPS 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 trade-off studies can be performed that can aid in the development of a more efficient design methodology for multi-element airfoil based IPS systems.
| Item Type: | Article |
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| Subjects: | Environmental Aerospace Mechanical |
| Depositing User: | Dr. FAROOQ SAEED |
| Date Deposited: | 30 Mar 2008 08:17 |
| Last Modified: | 01 Nov 2019 13:25 |
| URI: | http://eprints.kfupm.edu.sa/id/eprint/814 |