Infrared Technology, Volume. 43, Issue 6, 587(2021)

Numerical Simulation of Radiation Characteristics of Aircraft Exhaust Systems with Different Nozzles

Zhangbin HUANG1、*, Liu GUAN1, Xiaoxia LI2,3, and Yunsong FENG3
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    [1] [1] Aguiar P, Brett D, Brandon N P. Solid oxide fuel cell/gas turbine hybrid system analysis for high-altitude long-endurance unmanned aerial vehicles[J]. International Journal of Hydrogen Energy, 2008, 33(23): 7214-7223.

    [2] [2] Suresh Patel, Christopher Blac. Statistical modeling of F/A-22 flight test Buffet data for probabilistic analysis[C]// Aiaa/asme/asce/ahs/asc Structures, Structural Dynamics and Materials Conference, 2005: DOI: 10.2514/6.2005-2289.

    [3] [3] Roblin A, Baudoux P E, Chervet P. UV missile-plume signature model [C]//Proc of SPIE, 2002, 4718: 344-355.

    [4] [4] Bakker E J, Fair M L, Schleijpen H M A. Modeling multispectral imagery data with NIRATAM v3.1 and NPLUME v1.6 [C]// Proceedings of SPIE, 1999, 3699: 80-91.

    [5] [5] Watkins W R. Thermal background modeling and its use in science and technology[C]//Proceedings of SPIE, 1992, 1687: 84-106.

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    HUANG Zhangbin, GUAN Liu, LI Xiaoxia, FENG Yunsong. Numerical Simulation of Radiation Characteristics of Aircraft Exhaust Systems with Different Nozzles[J]. Infrared Technology, 2021, 43(6): 587

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    Paper Information

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    Received: Sep. 23, 2020

    Accepted: --

    Published Online: Aug. 26, 2021

    The Author Email: Zhangbin HUANG (408867079@qq.com)

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