Nonlinear aeroelastic behavior of a two-dimensional heated panel by irregular shock reflection considering viscoelastic damping  

Description

The dataset consists of raw data for the manuscript "Nonlinear aeroelastic behavior of a two-dimensional heated panel by irregular shock reflection considering viscoelastic damping" submitted to the Journal of Fluids and Structures. The dataset includes shock reflection boundary, aeroelastic stability boundary, aeroelastic response, bifurcation diagram, and proper orthogonal modes.

Institutions

• Northwestern Polytechnical University

  Shaanxi, Xi'an

Categories

Funders

• National Natural Science Foundation of China

  Beijing, China

  Grant ID: 12372233
• Fund of NPU-Duke China Seed Program

  Grant ID: 119003067
• '111 Project' of China

  Grant ID: B17037-106

Licence