• Infrared and Laser Engineering
  • Vol. 34, Issue 1, 42 (2005)
[in Chinese]1、*, [in Chinese]1, and [in Chinese]2
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    [in Chinese], [in Chinese], [in Chinese]. Theoretical calculations of infrared radiation of the projectile in flight[J]. Infrared and Laser Engineering, 2005, 34(1): 42 Copy Citation Text show less
    References

    [1] Dupuis A D,Edwards J A. Flight tests and computational analysis of two hypersonic research projectiles[A].33rd Aerospace Sciences Meeting and Exhibit[C]. American:American Inst of Aeronautics and Astronautics, 1995.1-11.

    [2] Clay W H. Theoretical temperature distribution in the precursor region ahead of projectiles traveling at hypersonic velocities[R].AD-718 641.1970.

    [3] Soencksen K P. Measurement of projectile surface temperature by means of its infrared radiation:a preliminary study[R]. AD-A264053.1993

    [6] Tofani A. Computer modeling of infrared head-on emission from missile noses[J]. Optical Engineering, 1990,29(2):87-96.

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    [in Chinese], [in Chinese], [in Chinese]. Theoretical calculations of infrared radiation of the projectile in flight[J]. Infrared and Laser Engineering, 2005, 34(1): 42
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