A Design Method in Robust Dynamic Boundary Protection System under Condition of Ice Formation on Aircraft by Differential Manifold Theory

LI Yinghui; GUI Yewei; ZUO Renwei; DONG Zehong; ZHANG Jiuxing

doi:10.3969/j.issn.1009-3516.2020.05.001

Home>Articles>A Design Method in Robust Dynamic Boundary Protection System under Condition of Ice Formation on Aircraft by Differential Manifold Theory

DOI: 10.3969/j.issn.1009-3516.2020.05.001

A Design Method in Robust Dynamic Boundary Protection System under Condition of Ice Formation on Aircraft by Differential Manifold Theory

LI Yinghui

GUI Yewei

ZUO Renwei

DONG Zehong

ZHANG Jiuxing

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Publication Date：2020-10-25

Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)

Pages：8( 1-8 )

Journal of Air Force Engineering University(Natural Science Edition)

PKUISTIC

ISSN：1009-3516

Year, Vol.(Issue)：2020,21(5)