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Numerical simulation of optical transmission through high speed aircraft optical window in aero-dynamic thermal environment

  • Zhi Gang Fan*
  • , Ya Ping Zhang
  • , Yang Wei Pei
  • , Jun Zhang
  • , Yan Lei He
  • *Corresponding author for this work
  • Harbin Engineering University
  • Harbin Institute of Technology

Research output: Contribution to journalArticlepeer-review

Abstract

In the aero-dynamic environment, optical window's shape and optical property will be changed because of thermal transmission and thermal stress, then the transmission of the infrared radiation from the target will be affected, which will make the image fuzzy, flutter, departure and energy's attenuation, thus, the effectiveness of infrared image will be heavily affected. According to the requirement of IR imaging technique applied in high-speed interceptor, the optical transmission theory and basic calculating methods of optical window were studied. The mathematic model and simulation software were introduced. Some computer simulation results at classical state were presented.

Original languageEnglish
Pages (from-to)396-400
Number of pages5
JournalHongwai Yu Haomibo Xuebao/Journal of Infrared and Millimeter Waves
Volume26
Issue number5
StatePublished - Oct 2007

Keywords

  • Aero-dynamic thermal
  • Air-optics
  • Optical window
  • Ray-tracing

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