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2011•Advanced materials researchRequires access

The Research on Aeroelasticity of the Vehicle Wing Surface

Zhi Ling Peng

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Abstract

By taking high aspect ratio straight wing as the research object, static aerodynamic force and dynamic aerodynamic force are detailed analysed and researched. The flutter speed of panel derived from Unsteady Theory and Theory.

About this research paper

What this paper is about

By taking high aspect ratio straight wing as the research object, static aerodynamic force and dynamic aerodynamic force are detailed analysed and researched. The flutter speed of panel derived from Unsteady Theory and Theory.

Why it matters

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Method / approach

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Available abstract

By taking high aspect ratio straight wing as the research object, static aerodynamic force and dynamic aerodynamic force are detailed analysed and researched. The flutter speed of panel derived from Unsteady Theory and Theory.

Key concepts: Aeroelasticity, Flutter, Wing, Aerodynamics, Structural engineering, Research Object, Aerodynamic force, Aerospace engineering

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