RESULT COMPARISON OF NUMERICAL ANALYSIS AND STRUCTURAL TESTS OF AEROSPACE TEST STRUCTURE

Journal Title: Prace Instytutu Lotnictwa - Year 2016, Vol 244, Issue 3

Abstract

The flaws resulting from the production process of fiber composite aerospace parts constitute a substantial problem for the exploitation safety of the structures. In the project TEBUK ‘Development of the technology for testing the resistance to damage of aviation and space composite load bearing structures’, which is carried out in the Institute of Aviation, the methodology which allows to predict the growth of the production flaws has been developed. The methodology was validated for the case of aerospace structure. A test structure referring to I-23 ‘Manager’ horizontal stabilizer was designed in order to validate the method. An artifitial production flaw – delamination, was placed in the test structure skin. During the structural tests the behaviour of the delamination and entire structure was recorded with the use of the strain gauges. In addition to the structural tests the FEM analyses aiming to model the behaviour of the structure and delamination were carried out. The FEM analysis results were compared to the results of the structural tests. The good cosistency between the results of the analyses and tests allowed to confirm the validyty of the analysis methods.<br/><br/>

Authors and Affiliations

Anna Osmęda

Keywords

Related Articles

Obliczenia flatteru prostokątnego płata ze sterem za pomocą MSC Nastran, ZONA ZAERO i ANSYS Fluent - porównanie z wynikami w tunelu aerodynamicznym

Do oceny właściwości aeroelastycznych obiektów latających powszechnie wykorzystywane sąanalizy obliczeniowe w dziedzinie częstości. W niniejszej pracy do sprawdzenia wiarygodnościtakich obliczeń wykorzystano wyniki badań...

ICT platform as a marketing tool of a scientific unit from the food-agricultural branch

In the age of dynamically developing market economy research and development units are treated as a kind of companies, which offer results of carried out scientific research projects. Currently, the potential of marketin...

A university's brand in the contemporary world

From the marketing perspective, clients buying branded products become marketing tools. They enhance the advertising of a given product or service. They join the ranks of people who give favourable opinions about the pro...

Social Media Marketing - why businesses need to use it and how (includes a study of Facebook)

Despite what some of the more luddite amongst others may wish, social media is a passing fad. Familiar social media websites like Facebook and Twitter are now as much a part of our daily lives as mobile phones.This paper...

Przegląd rozwiązań strukturalnych w zakresie ochrony struktur kompozytowych przed uderzeniem pioruna

Artykuł opisuje konstrukcje kompozytowe stosowane w lotnictwie, które narażone sąna wyładowania atmosferyczne. Zaprezentowano skutki wyładowania atmosferycznego w kontakciez kompozytem węglowym. Przedstawiono sposób ochr...

Download PDF file
  • EP ID EP186131
  • DOI 10.5604/05096669.1222764
  • Views 43
  • Downloads 0

How To Cite

Anna Osmęda (2016). RESULT COMPARISON OF NUMERICAL ANALYSIS AND STRUCTURAL TESTS OF AEROSPACE TEST STRUCTURE. Prace Instytutu Lotnictwa, 244(3), 125-136. https://europub.co.uk/articles/-A-186131