Large-attack-angle nonlinear separation flow aerodynamic force correction method

**The invention discloses a large-attack-angle nonlinear separation flow aerodynamic force correction method. The method comprises the following steps: obtaining aircraft surface pressure distribution data under zero reduction frequency by adopting a DES (Data Encryption Standard) method; performing...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHANG TAO, ZHENG HONGTAO, QIU FENG, ZHANG MANG, XIE HAIOU, MA YUANHONG, WAN SHUANG, HU GUOTUN, SHI SHUO, SHI WEI, ZHANG JING, SUN BING, LI XIAOYAN, LIU JIEPING, LI HUAGUANG, RONG HUA, PARK CHOONG-GEOL, MENG QUNZHI, LYU JINAN, CHENG LIN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CALCULATING COMPUTING COUNTING ELECTRIC DIGITAL DATA PROCESSING PHYSICS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!