Journal of Aerospace System Engineering (항공우주시스템공학회지)
- Volume 8 Issue 1
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- Pages.30-35
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- 2014
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
DOI QR Code
Development of an Ejector System for the Engine-Bay Ventilation
엔진베이 환기용 이젝터시스템 개발
- Received : 2013.11.11
- Published : 2014.03.31
Abstract
This study has been conducted to develop an ejector system applied in the aircraft engine-bay ventilation system. Tandem-Ejector was selected as a component of ventilation system because it could achieve high ventilation performance in spite of motive flow with small flow rate. Tandem-Ejector is composed of a primary nozzle and two mixing ducts (
Keywords
- Engine-Bay Ventilation System;
- Tandem-Ejector System;
- Ejector Nozzle;
- Mixing Duct;
- Sizing Design;
- 1-D Analysis;
- CFD Analysis