夹层结构蜂窝芯的柔度分析

Q4 Engineering

Fatigue of Aircraft Structures Pub Date : 2019-12-01 DOI:10.2478/fas-2019-0003

D. Nowakowski, Marta Baran, J. Lisiecki, S. Kłysz, P. Synaszko

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引用次数: 0

摘要

摘要本文的研究目的是确定米格-29战斗机水平尾翼夹层结构在静压缩试验中的蜂窝芯柔度。试件的研究依据ASTM C365/C365M标准进行。本文介绍了实验确定的依赖关系和强度参数的结果，即力-位移依赖关系，压缩模量和蜂窝芯变形。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Examination of Honeycomb Core Compliance in Sandwich Structure

Abstract The objective of the research presented in this paper was to determine the honeycomb core compliance of a sandwich structure of the horizontal stabilizer of the MiG-29 fighter jet in the static compression test. The study of the specimen was conducted based on the ASTM C365/C365M standard. The article presents the results of experimentally determined dependencies and strength parameters, i.e. the force-displacement dependence, the compressive modulus and the honeycomb core deformations.

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来源期刊

Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality

CiteScore

0.40

自引率

0.00%

发文量

期刊介绍： The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.