Proceedings of the KSME Conference (대한기계학회:학술대회논문집)
- 2002.08a
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- Pages.271-274
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- 2002
The high altitude test method of Scramjet engine combustor model
스크램제트 연소기 모델의 고공시험 연구
- Woo Kwan Je ;
- Kim Young Soo ;
- Skivin V. A
- Published : 2002.08.01
Abstract
This paper is investigated construction of the Scramjet test facility and test method of Scramjet engine combustor model. Scramiet engine combustor model test was performed at Lab C-16BK CIAM (Central Institute of Aviation Motors) at Tyraevo in Moscow. The velocity of flow in the combustion chamber equal to Mach number 2.49 with single hole fuel spray nozzle injector and test duration equal to 7 seconds. Therefore In this paper is showed high altitude test method of Scramjet combustor model and the proper structure of combustor with single hole fuel spray nozzle.
Keywords
- Scramjet test facility;
- test method of Scramjet engine combustor model;
- single hole fuel spray nozzle injector