An Analysis Method for Inertial Particle Separator
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 dropl...
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| Other Authors: | , |
| Format: | article |
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2007
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| Online Access: | https://eprints.kfupm.edu.sa/id/eprint/814/1/20245_proof1.pdf |
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| _version_ | 1864513389206700032 |
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| author | Saeed, Farooq |
| author2 | Al-Garni, Ahmed Z. unknown |
| author2_role | author author |
| author_facet | Saeed, Farooq Al-Garni, Ahmed Z. unknown |
| author_role | author |
| dc.creator.none.fl_str_mv | Saeed, Farooq Al-Garni, Ahmed Z. unknown |
| dc.date.none.fl_str_mv | 2007-07-01 2020 |
| dc.format.none.fl_str_mv | application/pdf |
| dc.identifier.none.fl_str_mv | https://eprints.kfupm.edu.sa/id/eprint/814/1/20245_proof1.pdf (2007) An Analysis Method for Inertial Particle Separator. AIAA Journal of Aircraft, 44 (4). pp. 1150-1158. |
| dc.language.none.fl_str_mv | en |
| dc.publisher.none.fl_str_mv | AIAA |
| dc.relation.none.fl_str_mv | https://eprints.kfupm.edu.sa/id/eprint/814/ |
| dc.rights.*.fl_str_mv | info:eu-repo/semantics/openAccess |
| dc.subject.none.fl_str_mv | Environmental Aerospace Mechanical |
| dc.title.none.fl_str_mv | An Analysis Method for Inertial Particle Separator |
| dc.type.none.fl_str_mv | Article PeerReviewed info:eu-repo/semantics/publishedVersion info:eu-repo/semantics/article |
| description | 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. |
| eu_rights_str_mv | openAccess |
| format | article |
| id | KFUPM_74c19e4f7585832d5c85a9a26088aee1 |
| identifier_str_mv | (2007) An Analysis Method for Inertial Particle Separator. AIAA Journal of Aircraft, 44 (4). pp. 1150-1158. |
| language_invalid_str_mv | en |
| network_acronym_str | KFUPM |
| network_name_str | King Fahd University of Petroleum and Minerals |
| oai_identifier_str | oai::814 |
| publishDate | 2007 |
| publisher.none.fl_str_mv | AIAA |
| repository.mail.fl_str_mv | |
| repository.name.fl_str_mv | |
| repository_id_str | |
| spelling | An Analysis Method for Inertial Particle SeparatorSaeed, FarooqAl-Garni, Ahmed Z.unknownEnvironmentalAerospaceMechanicalThe 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.AIAA2007-07-012020ArticlePeerReviewedinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttps://eprints.kfupm.edu.sa/id/eprint/814/1/20245_proof1.pdf (2007) An Analysis Method for Inertial Particle Separator. AIAA Journal of Aircraft, 44 (4). pp. 1150-1158. enhttps://eprints.kfupm.edu.sa/id/eprint/814/info:eu-repo/semantics/openAccessoai::8142019-11-01T13:25:22Z |
| spellingShingle | An Analysis Method for Inertial Particle Separator Saeed, Farooq Environmental Aerospace Mechanical |
| status_str | publishedVersion |
| title | An Analysis Method for Inertial Particle Separator |
| title_full | An Analysis Method for Inertial Particle Separator |
| title_fullStr | An Analysis Method for Inertial Particle Separator |
| title_full_unstemmed | An Analysis Method for Inertial Particle Separator |
| title_short | An Analysis Method for Inertial Particle Separator |
| title_sort | An Analysis Method for Inertial Particle Separator |
| topic | Environmental Aerospace Mechanical |
| url | https://eprints.kfupm.edu.sa/id/eprint/814/1/20245_proof1.pdf |