Infrared and Laser Engineering, Volume. 49, Issue 7, 20190520(2020)

Simulation analysis of influence of aerodynamic heating effect of dome window on rosette scan system

Yinhuan Lv
Author Affiliations
  • 中国科学院上海技术物理研究所,上海 200083
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    References(14)

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    [3] R D Firouz-Abadi, S M Alavi, H Salarieh. Analysis of non-linear aeroelastic response of a supersonic thick fin with plunging, pinching and flapping free-plays. Fluids and Structures, 163-184(2013).

    [8] E Başkut, A Akgül. Development of a coupling crocedure for static aeroelastic analyses. Scientific Technical Review, 61, 39-48(2011).

    [15] [15] Xerikos J, Rose W C, Rawlinson, et al. Measurement of mean fluctuating flow properties in hypersonic shear layers[R]. Virginia: AIAA, 1990: 901409.

    [16] Yuanchun Liu, Yurong He, Jiaqi Zhu. Numerical simulation of aerodynamic heating and stresses of chemical vapor deposition ZnS for hypersonic vehicles. Journal of Zhejiang University Science A (Appl Phys & Eng), 15, 185-196(2014).

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    Paper Information

    Category: 红外技术及应用

    Received: Oct. 18, 2019

    Accepted: Dec. 13, 2019

    Published Online: Aug. 19, 2020

    The Author Email:

    DOI:10.3788/IRLA20190520

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