• Title/Summary/Keyword: 항공기 플룸 저부가열

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Effects of Flight Conditions on IR Signature from Aircraft Exhaust Plume (비행조건에 따른 항공기 배기플룸의 IR 신호 특성)

  • Go, Gun-Yung;Kim, Man-Young;Baek, Seung-Wook
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.5
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    • pp.58-66
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    • 2012
  • The IR signature and radiative base heating from an aircraft plume have been important factors for aircraft survivability in modern battle fields. In order to enhance the aircraft survivability and reduce the base heating, infrared signatures emitted from an aircraft exhaust plume should be determined. In this work, therefore, IR signatures and radiative base heating characteristics are examined in the plume exhausted from the aircraft with operating at altitude of 5 km in M=0.9 and 1.6, respectively. As a result, it is found that the particular wavelength IR signature has high spectral characteristics because of $H_2O$ and $CO_2$ gases in the plume, and the radiative heat flux coming into the base plane increases with higher Mach number and shorter distance.

Effects of Flight Conditions on IR Signature from Aircraft Exhaust Plume (비행조건에 따른 항공기 배기플룸의 IR 신호 특성)

  • Go, Gun-Yung;Kim, Man-Young;Baek, Seung-Wook
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2012.05a
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    • pp.282-289
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    • 2012
  • The IR Signature and radiative base heating from an aircraft plume have been important factors for aircraft survivability in modern battle fields. In order to enhance the aircraft survivability and reduce the base heating, infrared signatures emitted from an aircraft exhaust plume should be determined. In this work, therefore, IR signatures and radiative base heating characteristics are examined in the plume exhausted from the aircraft with operating at altitude of 5km in M=0.9 and 1.6, respectively. As a result, it is found that the particular wavelength IR signature has high spectral characteristics because of $H_2O$ and $CO_2$ gases in the plume, and the radiative heat flux coming into the base plane increases with higher Mach number and shorter distance.

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Investigation of the Radiative Heating from Aircraft Plume with Particles (입자에 의한 항공기 플룸의 열복사 가열에 관한 연구)

  • Go, Gun-Yung;Yi, Kyung-Joo;Lee, Sung-Nam;Kim, Won-Cheol;Baek, Seung-Wook;Kim, Man-Young
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.9
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    • pp.737-744
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    • 2012
  • The finite volume method for radiation is applied for the analysis of radiative base heating by SE and PE of the aircraft exhaust plume. The exhaust plume is considered as an absorbing, emitting, and scattering medium, while the base plane is assumed to be cold and black. The radiative properties of non-gray gases are obtained through the WSGGM, and the particle is modelled as spheres. The present method is validated by comparing the results with those of the backward Monte-Carlo method and then the radiative base heating characteristics are analyzed by changing such various parameters as particle concentration, temperature, and scattering phase function. The results show that the radiative heat flux coming into the base plane decreases with altitude and distance, but it increases as the particle temperature increases. The forward scattering of particles increases PE while it decreases SE.