Propeller slipstream effect uncertainty obtaining method based on random polynomial chaos expansion

The invention discloses a propeller slipstream effect uncertainty obtaining method based on random polynomial chaos expansion. The method comprises the following steps: firstly, carrying out statistics on each moment of an uncertainty variable in the flight process of the propeller-driven aircraft;...

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Bibliographische Detailangaben
Hauptverfasser: LI GEN, ZHANG PEIHONG, QIU JINGXUAN, ZUO LINGYU, LI YAO, ZHAO WEI, WU XIAOJUN, SI HAIQING
Format: Patent
Sprache:chi ; eng
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