Work

The compression properties of the wing integral panel made up of material 7B50-T7751 and 7150-T7751

Year: 2019

Type: article

Abstract: The integral panel is significant structure of modern advanced aircraft. Stability is one of the most important problems of aircraft structure design. This paper focused on the compression properties of the material 7B50-T7751 and 7150-T7751. According to the engineering algorithm, we got the compression result of the wing integral panel. By the experimental study, we can obtain the load-strain curves of the two integral panel forms. The comparison of the compression properties provides a basis to the choice of integral panel.

Source: International Journal of Lightweight Materials and Manufacture

DOI: 10.1016/j.ijlmm.2019.08.007

Authors: Yuanbo Lv, Wendong Zhang, Yulong Wei

Institutions: Aviation Industry Corporation of China (China), Aircraft Strength Research Institute (China)

Language: English

Topic: Cellular and Composite Structures

Subfield: Mechanical Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: diamond

OpenAlex ID: W2971027751

FWCI:

Cites: 1

Cited by: 2

Related to: 10