AEROSPACE SHANGHAI, Volume. 42, Issue 1, 169(2025)

Effects of Injection Gases on High-temperature Hypersonic Laminar/turbulent Boundary Layer Flow

Xinyi WU*... Lun ZHANG, Yuqiu ZHANG, Zhongzheng JIANG, Changju WU and Weifang CHEN |Show fewer author(s)
Author Affiliations
  • School of Aeronautics and Astronautics,Zhejiang University,Hangzhou310027,,China
  • show less
    References(19)

    [13] C Y WANG, W W LIOU, S X XU. Skin-friction prediction for high-speed turbulent boundary layers with ablation. Journal of Spacecraft and Rockets, 41, 893-895(2004).

    [15] Y SUMITANI, N KASAGI. Direct numerical simulation of turbulent transport with uniform wall injection and suction. AIAA Journal, 33, 1220-1228(1995).

    [16] E ORLIK, I FEDIOUN, N LARDJANE. Hypersonic boundary-layer transition forced by wall injection:a numerical study. Journal of Spacecraft and Rockets, 51, 1306-1318(2014).

    [17] H JOHNSON, J GRONVALL, G V CANDLER. Reacting hypersonic boundary layer stability with blowing and suction(2009).

    [18] J E BARTH, V WHEATLEY, M K SMART. Hypersonic turbulent boundary-layer fuel injection and combustion:skin-friction reduction mechanisms. AIAA Journal, 51, 2147-2157(2013).

    [19] F M MIRÓ, F PINNA. Injection-gas-composition effects on hypersonic boundary-layer transition, 4-14(2020).

    [21] Z X GAO, C W JIANG, S W PAN et al. Combustion heat-release effects on supersonic compressible turbulent boundary layers. AIAA Journal, 53, 1949-1968(2015).

    [22] Y LIU, Y ZHANG, W WANG et al. Hypersonic boundary layer flow and heat transfer analysis of compressible fluid over a permeable wall with gas injection. International Communications in Heat and Mass Transfer:A Rapid Communications Journal, 129, 105688(2021).

    [25] L ZHANG, Z Z JIANG, Y L QIU et al. Direct numerical simulations of first-mode oblique breakdown in a supersonic boundary layer under wall tran-spiration. Aerospace Science and Tecnology, 150, 109165(2024).

    [26] M G DUNN, W S KANG. Theoretical and experimental studies of reentry plasmas.

    [27] C PARK, R L JAFFE, H PARTRIDGE. Chemical-knetic parameters of hyperbolic earth entry. Journal of Thermophysics and Heat Transfer, 15, 76-90(2001).

    [28] F G BLOTTNER. Viscous shock layer at the stagnation point with nonequilibrium air chemistry. AIAA Journal, 7, 2281-2288(1969).

    [29] R GUPTA, R THOMPSON et al. A review of reaction rates and thermodynamic and transport properties for an 11-species air model for chemical and thermal nonequilibrium calculations to 30000K:NASA RP-1232.

    [30] C PARK. Review of chemical-kinetic problems of future NASA missions.I:Earth entries. Journal of Thermophysics and Heat Transfer, 7, 385-398(1993).

    [31] C PARK, J T HOWE, R L JAFFE et al. Review of chemical-kinetic problems of future NASA missions.Ⅱ:Mars entries. Journal of Thermophysics and Heat Transfer, 8, 9-23(1994).

    [32] N COHEN, K WESTBERG. Evaluation and compilation of chemical kinetic data. The Journal of Physical Chemistry, 83, 46-50(1979).

    [33] R THOMPSON, P GNOFFO. Implementation of a blowing boundary condition in the LAURA Code:AIAA-2008-1243(2008).

    [34] A MARTIN, I BOYD. Modeling of heat transfer attenuation by ablative gases during the Stardust re-entry. Journal of Thermophysics and Heat Transfer, 3, 450-466(2012).

    [35] Q YOU, X F YANG, L ZENG et al. Coupled heat transfer characteristics on chemically reacting interface of high-speed aircraft considering wall injection(2021).

    Tools

    Get Citation

    Copy Citation Text

    Xinyi WU, Lun ZHANG, Yuqiu ZHANG, Zhongzheng JIANG, Changju WU, Weifang CHEN. Effects of Injection Gases on High-temperature Hypersonic Laminar/turbulent Boundary Layer Flow[J]. AEROSPACE SHANGHAI, 2025, 42(1): 169

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category: Speciality Discussion

    Received: Dec. 6, 2024

    Accepted: --

    Published Online: May. 13, 2025

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2025.01.018

    Topics