AEROSPACE SHANGHAI, Volume. 41, Issue 4, 11(2024)

Analysis on Heat Transfer Characteristics of Film-based Structures with Temperature Sensitive Paint in Hypersonic Wind Tunnels

Yanheng ZHANG... Yu ZHUANG, Dong ZHI, Shouchao HU and Tao JIANG |Show fewer author(s)
Author Affiliations
  • Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang621000,, China
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    References(10)

    [6] S OHMI, H NAGAI, K ASAI. Effect of TSP layer thickness on global heat transfer measurement in hypersonic flow:AIAA 2006-1048(2006).

    [10] S G HAN, G WU, J GONG et al. Phosphor thermography for global heat transfer measurement in gun tunnel:AIAA 2013-0486(2013).

    [20] N TAKEHIRO, N HIROKI. Visualization of hypersonic boundary layer transition on elliptic cone in high enthalpy shock tunnel with temperature-sensitive paint:AIAA 2016-0358(2016).

    [22] T LIU, Z CAI, J LAI. Analytical methods for determination of heat transfer fields from temperature sensitive paint measurements in hypersonic tunnels:AIAA 2009-736(2009).

    [23] T LIU, B WANG, J RUBAL et al. Correcting lateral heat conduction effect in image-based heat flux measurements as an inverse problem. International Journal of Heat and Mass Transfer, 54, 1244-1258(2011).

    [24] X LIU, H SHAO, W ZHOU et al. Apparent temperature in temperature-sensitive paint measurement and its effect on surface heat flux determination for hypersonic flows. Measurement Science and Technology, 31, 125302(2020).

    [25] D PENG, L JIAO, Z SUN et al. Simultaneous PSP and TSP measurements of transient flow in a long‑duration hypersonic tunnel. Experiments in Fluids, 57, 188(2016).

    [27] T LIU, J MONTEFORT, S STANFIELD et al. Inverse heat transfer methods for global heat flux measurements in aerothermodynamics testing. Progress in Aerospace Sciences, 107, 1-18(2019).

    [29] Z CAI, T LIU, B WANG et al. Numerical inverse heat transfer analysis for temperature-sensitive-paint measurements in hypersonic tunnels. Journal of Thermophysics and Heat Transfer, 25, 59-67(2011).

    [30] H TAKEHITO, N HIROKI. Development of temperature-sensitive paint with high performance and responsivity for aerodynamic heating measurement:AIAA 2014-1408(2014).

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    Yanheng ZHANG, Yu ZHUANG, Dong ZHI, Shouchao HU, Tao JIANG. Analysis on Heat Transfer Characteristics of Film-based Structures with Temperature Sensitive Paint in Hypersonic Wind Tunnels[J]. AEROSPACE SHANGHAI, 2024, 41(4): 11

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    Paper Information

    Category: Aerospace Aerodynamics and Test Technology

    Received: Jan. 4, 2024

    Accepted: --

    Published Online: Nov. 18, 2024

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.04.002

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