• Journal of Infrared and Millimeter Waves
  • Vol. 24, Issue 2, 125 (2005)
[in Chinese], [in Chinese], and [in Chinese]
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  • [in Chinese]
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    DOI: Cite this Article
    [in Chinese], [in Chinese], [in Chinese]. MODEL EXPERIMENTS OF INFRARED SUPPRESSOR FOR HELICOPTER EXHAUST SYSTEM[J]. Journal of Infrared and Millimeter Waves, 2005, 24(2): 125 Copy Citation Text show less
    References

    [1] Francois T. Internal aerodynamics of infrared suppressors for helicopter engines [C]. 40th Annual National Forum of the American Helicopter Society, 1984:1-14.

    [2] Power G D, McClure M D, Vinh D. Advanced IR suppressor design using a combined CFD/test approach [R]. AIAA Paper, 94-3215,1994.

    [4] Presz W M, Gousy R G, Morin B L. Forced mixer lobes in ejector designs [R]. AIAA Paper 86-1614,1986.

    [5] Presz W M, Morin B L, Blinn R F. Short efficient ejector systems [R]. AIAA Paper 1987,87-1837.

    [6] Liu Y H. Experimental and numerical investigation of circularly lobed nozzle with/without central plug [J]. International Journal of Heat and Mass Transfer, 2002,45(13):2577-2585.

    [7] Zhang Jing-Zhou, Xie Zhi-Rong. Three-dimensional computational study for flow fields within fored lobe mixer [R]. ISABE-2003-1104,2003.

    [8] Birk A M, Vandam D. Infrared signature suppression for marine gas turbine:comparison of sea trail and model test result for the DRES IRSS system [J]. ASMA Journal of Engineering for Gas Turbines and Power, 1994,116(1):75-81.

    [in Chinese], [in Chinese], [in Chinese]. MODEL EXPERIMENTS OF INFRARED SUPPRESSOR FOR HELICOPTER EXHAUST SYSTEM[J]. Journal of Infrared and Millimeter Waves, 2005, 24(2): 125
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