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Experimental research on boundary layer behaviors of ultra-high-lift low-pressure turbine profile based on surface-mounted hot-film
更新时间：2026-07-07

    • Experimental research on boundary layer behaviors of ultra-high-lift low-pressure turbine profile based on surface-mounted hot-film

    • Vol. 26, Issue 1, (2011)

    • Published：2011

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  • LI Wei, ZHU Jun-qiang, LI Gang, et al. Experimental research on boundary layer behaviors of ultra-high-lift low-pressure turbine profile based on surface-mounted hot-film[J]. 2011, 26(1). DOI：

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Related Author

LI Wei
ZHANG Bo
ZHOU Min
LU Xin-gen
ZHU Jun-qaing
LIANG Yun
LIU Huo-xing
ZOU Zheng-ping

Related Institution

Key Laboratory of Light-duty Gas-turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences
Beijing Aviation Engineering Research Center
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Collaborative Innovation Center for Advanced Aero-Engine
Institute of Systems Engineering,Academy of Military Sciences,the Chinese People’s Liberation Army
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