Structural Deformation-Based Computational Method for Static Aeroelasticity of High-Aspect-Ratio Wing Model in Pressurized Wind Tunnel

DOI10.4208/AAMM.OA-2017-0342zbMath1488.74051OpenAlexW2917852494WikidataQ128361777 ScholiaQ128361777MaRDI QIDQ5156611

Li Ding, Ennan Shen, Zhiliang Lu, Tongqing Guo

Publication date: 11 October 2021

Published in: Advances in Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.4208/aamm.oa-2017-0342

zbMATH Keywords

structural stiffnesshigh-aspect-ratio wingCFD-CSDpressurized wind tunnelstatic aeroelastic computation

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Spectral, collocation and related methods for initial value and initial-boundary value problems involving PDEs (65M70) Mesh generation, refinement, and adaptive methods for the numerical solution of initial value and initial-boundary value problems involving PDEs (65M50)

Uses Software

• Spalart-Allmaras

Cites Work

• Static aeroelastic analysis of a high-aspect-ratio wing based on wind-tunnel experimental aerodynamic forces
• A TIME-DOMAIN METHOD FOR TRANSONIC FLUTTER ANALYSIS WITH MULTIDIRECTIONAL COUPLED VIBRATIONS

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