Analysis of Static Aeroelastic Characteristics of Distributed Propulsion Wing

Analysis of Static Aeroelastic Characteristics of Distributed Propulsion Wing

The static aeroelastic characteristics of the distributed propulsion wing (DPW) were studied using the CFD/CSD loose coupling method in this study. The momentum source method of the Reynolds-averaged Navier–Stokes equation based on the k-ω SST turbulence model solution was used as the CFD solution m...

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Bibliographic Details
Main Authors: Junlei Sun, Zhou Zhou, Tserendondog Tengis, Huailiang Fang
Format: Article
Language:English
Published: MDPI AG 2024-12-01
Series:Aerospace
Subjects:
distributed propulsion wing (DPW)
static aeroelastic analysis
parametric modeling
loosely coupled
equivalent airfoil
Online Access:https://www.mdpi.com/2226-4310/11/12/1045
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