Analysis method for inertial particle separator

被引：0
|
作者：
Saeed, Farooq [1 ,2 ,3 ]
Al-Garni, Ahmad Z. [1 ,3 ,4 ]
机构：
[1] King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi Arabia
[2] Aerospace Engineering Department, KFUPM, Mail Box 1637, Saudi Arabia
[3] AIAA, United States
[4] Aerospace Engineering Department, KFUPM, Mail Box 842, Saudi Arabia
来源：
Journal of Aircraft | 1600年 / 44卷 / 04期
关键词：
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;
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摘要：
Conference article (CA)
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页码：1150 / 1158
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