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Experimental investigation of infrared signal characteristics in a micro-turbojet engine

Authors
명노신Choi, SM (Choi, S. M.)Myong, S (Myong, S.)Kim, W (Kim, W.)
Issue Date
Mar-2019
Publisher
Royal Aeronautical Society
Citation
Aeronautical Journal, v.123, no.1261, pp 340 - 355
Pages
16
Indexed
SCIE
SCOPUS
Journal Title
Aeronautical Journal
Volume
123
Number
1261
Start Page
340
End Page
355
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/9366
ISSN
0001-9240
2059-6464
Abstract
Infrared signal measurements from a micro-turbojet engine are conducted to understand the characteristics of the engine performance and the infrared signal by varying the exhaust nozzle configuration. A cone type nozzle and five rectangle type nozzles whose aspect ratios vary from one to five are used for this experimental work. As a result, it is confirmed that the thrust and the fuel consumption rate of the engine do not change greatly by varying the exhaust nozzle shape. In the case of the aspect ratio of 5, the specific fuel consumption of the engine is increased by about 3% compared to the reference cone nozzle, but the infrared signal can be reduced by up to 14%. As a result of measuring the temperature distribution of the plume gas, the correlation of infrared signal with plume gas temperature distribution can be understood. In the case of a cone shape, the distribution of plume gas formed to circular shape, and the high-temperature core region of plume gas continued to develop farther to the downstream. However, the temperature distribution was maintained in the rectangular shape as the aspect ratio increased, and the average temperature decreased sharply. As the aspect ratio increases, the plume spreads more widely.
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