High-speed boundary layer transition criterion calibration method and system based on flight test data

The invention discloses a high-speed boundary layer transition criterion calibration method based on flight test data. The method comprises the following steps: S1, acquiring a basic flow layer flow field of an aircraft by adopting a numerical simulation method; s2, carrying out boundary layer flow...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHAN ZHENLIN, MIAO MENG, ZHOU NAIZHEN, HUANG JIANDONG, TIAN CHUAN, GAO YUAN, CAI RUI, DUAN YI, SONG RUNJIE, YANG PAN, RAO CAIYAN, YAO SHIYONG, LI SIYI, CHEN ZHENG, ZHANG BEIZHAN, HE ZHENGGUANG
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!