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Analysis of MWIR and LWIR Signature of Supersonic Aircraft to Air-to-air and Surface-to-air Missile by Coupled Simulation Method

통합해석기법을 활용한 공대공 및 지대공 적외선 미사일 대응 초음속 항공기의 중적외선 및 원적외선 신호 분석

  • Kim, Taehwan (Department of Mechanical Engineering, Yonsei University) ;
  • Bae, Ji-Yeul (Department of Mechanical Engineering, Yonsei University) ;
  • Kim, Taeil (Department of Mechanical Engineering, Yonsei University) ;
  • Jung, Daeyoon (The 3rd Research and Development Institute, Agency for Defense Development) ;
  • Hwang, Chang Su (Department of Physics, Republic of Korea Air Force Academy) ;
  • Cho, Hyung Hee (Department of Mechanical Engineering, Yonsei University)
  • 김태환 (연세대학교 기계공학과) ;
  • 배지열 (연세대학교 기계공학과) ;
  • 김태일 (연세대학교 기계공학과) ;
  • 정대윤 (국방과학연구소 제3기술연구본부) ;
  • 황창수 (공군사관학교 물리학과) ;
  • 조형희 (연세대학교 기계공학과)
  • Received : 2014.06.10
  • Accepted : 2014.11.07
  • Published : 2014.12.05

Abstract

The stealth performance of supersonic aircraft in recent air battlefield is one of the most significant feature for latest fighters. Especially, as the technology is advancing, the IR stealth capability becomes more important because of its passive characteristic. To design an aircraft with stealth capability, we must know how much the IR signature is generated from the aircraft. Also, predicting the IR signature of enemy's aircraft is tactically crucial. In this study, we calculated MWIR and LWIR infrared signature of $5^{th}$ generation supersonic aircraft against air-to-air and surface-to-air threat using IR simulation code and CFD coupled procedure.

Keywords

References

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Cited by

  1. Susceptibility of combat aircraft modeled as an anisotropic source of infrared radiation vol.52, pp.5, 2016, https://doi.org/10.1109/TAES.2016.150513