Investigation on the Reynolds Number Effect of a Flying Wing Model with Large Sweep Angle and Small Aspect Ratio

Investigation on the Reynolds Number Effect of a Flying Wing Model with Large Sweep Angle and Small Aspect Ratio

The effect of the Reynolds number on the flying wing common research model with a large sweep angle and small aspect ratio is studied by numerical simulation. The helicity cross-flow transition correction of the Langtry–Menter model is established in view of the deficient prediction accuracies of ex...

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Bibliographic Details
Main Authors: Peng Lin, Jifei Wu, Lianshan Lu, Neng Xiong, Dawei Liu, Jichuan Su, Guangyuan Liu, Yang Tao, Junqiang Wu, Xueqiang Liu
Format: Article
Language:English
Published: MDPI AG 2022-09-01
Series:Aerospace
Subjects:
transonic flow
transition
Reynolds number
cross-flow transition
friction drag
Online Access:https://www.mdpi.com/2226-4310/9/9/523

Internet

https://www.mdpi.com/2226-4310/9/9/523

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