Structural Strength Analysis and Optimization of Commercial Aircraft Nose Landing Gear under Towing Taxi-Out Conditions Using Finite Element Simulation and Modal Testing.

Saved in:
Bibliographic Details
Title: Structural Strength Analysis and Optimization of Commercial Aircraft Nose Landing Gear under Towing Taxi-Out Conditions Using Finite Element Simulation and Modal Testing.
Authors: Lin, Qiwei1,2,3, lin2581451894@gmail.com, Yang, Chang4, Bai, Yuhao1,2,3, byh140624@163.com, Qin, Jiahao1,2,3, jhqin@cauc.edu.cn
Source: Aerospace (MDPI Publishing); May2024, Vol. 11 Issue 5, p414, 20p
Database: Applied Science & Technology Source
Description
ISSN:22264310
DOI:10.3390/aerospace11050414