초음속 항공기 전방위 탐지각도에 따른 적외선 피격성 분석IR Susceptibility of Supersonic Aircraft according to Omni-directional Detection Angle
- Other Titles
- IR Susceptibility of Supersonic Aircraft according to Omni-directional Detection Angle
- Authors
- 남주영; 장인중; 박경수; 조형희
- Issue Date
- Dec-2021
- Publisher
- 한국군사과학기술학회
- Keywords
- Supersonic Aircraft(초음속 항공기); IR Signature(적외선 신호); Susceptibility(피격성); Numerical Analysis (수치 해석)
- Citation
- 한국군사과학기술학회지, v.24, no.6, pp 638 - 644
- Pages
- 7
- Journal Title
- 한국군사과학기술학회지
- Volume
- 24
- Number
- 6
- Start Page
- 638
- End Page
- 644
- URI
- https://yscholarhub.yonsei.ac.kr/handle/2021.sw.yonsei/22906
- DOI
- 10.9766/KIMST.2021.24.6.638
- ISSN
- 1598-9127
- Abstract
- Infrared guided weapons act as threats that greatly degrade the survivability of combat aircraft. Infrared weapons detect and track the target aircraft by sensing the infrared signature radiated from the aircraft fuselage. Therefore, in this study, we analyzed the infrared signature and susceptibility of supersonic aircraft according to omni-directional detection angle. Through the numerical analysis, we derived the surface temperature distribution of fuselage and omni-directional infrared signature. Then, we calculated the detection range according to detection angle in consideration of IR sensor’s parameters. Using in-house code, the lethal range was calculated by considering the relative velocity between aircraft and IR missile. As a result, the elevational susceptibility is larger than the azimuthal susceptibility, and it means that the aircraft can be attacked in wider area at the elevational situation.
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Collections - College of Engineering > Mechanical Engineering > 1. Journal Articles
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