Receptivity and Stability Theory Analysis of a Transonic Swept Wing Experiment

Surface suction provides an efficient way to delay boundary layer transitions. In order to verify the suction effects and determine the mechanism of suction control in transonic swept wing boundary layers, wind tunnel transition measurements in a hybrid laminar flow control (HLFC) wind tunnel model...

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Bibliographic Details
Main Authors: Yuanqiang Liu, Yan Liu, Zubi Ji, Yutian Wang, Jiakuan Xu
Format: Article
Language:English
Published: MDPI AG 2023-10-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/10/903