Výsledky vyhledávání - "Kłysz Sylwester"

Akademický článek

Mechanical Tests Applied to Structural Health Monitoring: An Overview of Previous Experience

Autor: Baran Marta, Nowakowski Dominik, Lisiecki Janusz, Kłysz Sylwester

Publikováno v: Fatigue of Aircraft Structures, Vol 2020, Iss 12, Pp 123-135 (2020)

Laboratory for Materials Strength Testing (LMST) has been conducting accredited mechanical research for aviation from 2003. Among accredited procedures are e.g. low and high cycle fatigue tests, fracture toughness tests and fatigue crack growth rate

Externí odkaz: https://doaj.org/article/f8d1e06ab570446d89995af6707bee44

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Akademický článek

Comparative Study on Fatigue Life of CFRP Composites with Damages

Autor: Baran Marta, Synaszko Piotr, Lisiecki Janusz, Kłysz Sylwester

Publikováno v: Fatigue of Aircraft Structures, Vol 2019, Iss 11, Pp 28-38 (2019)

In this work, the compressive residual strength tests results, Compression After Impact (CAI), are presented. The specimens were made of carbon-epoxy prepreg E722-02 UHS 130-14. Two variants of specimens were tested: samples undamaged and samples wit

Externí odkaz: https://doaj.org/article/619d63dde06a4c6aa0b744a51de541a5

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Akademický článek

Examination of Honeycomb Core Compliance in Sandwich Structure

Autor: Nowakowski Dominik, Baran Marta, Lisiecki Janusz, Kłysz Sylwester, Synaszko Piotr

Publikováno v: Fatigue of Aircraft Structures, Vol 2019, Iss 11, Pp 19-27 (2019)

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 conducte

Externí odkaz: https://doaj.org/article/51067516d6ff408c8924a51fdb053bad

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Akademický článek

An On-Line Multiway Approach to In-Situ NDI Looking at the PZL-130TCII

Autor: Dragan Krzysztof, Dziendzikowski Michał, Kurnyta Artur, Latoszek Adam, Leski Andrzej, Kłysz Sylwester

Publikováno v: Fatigue of Aircraft Structures, Vol 2013, Iss 5, Pp 5-11 (2014)

Providing a reliable and universal Structural Health Monitoring (SHM) system allowing for remote aircraft inspections and a reduction of maintenance costs is a major challenge confronting the aerospace industry today. SHM based on guided Lamb waves i

Externí odkaz: https://doaj.org/article/66fbaef9323b4f89ae0bf474b803f625

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Akademický článek

An Approach to Structural Health Monitoring of Composite Structures Based on Embedded PZT Transducers

Autor: Dziendzikowski Michał, Dragan Krzysztof, Kurnyta Artur, Kornas Łukasz, Latoszek Adam, Zabłocka Magdalena, Kłysz Sylwester, Leski Andrzej, Chalimoniuk Marek, Giewoń Janusz

Publikováno v: Fatigue of Aircraft Structures, Vol 2014, Iss 6, Pp 113-118 (2014)

One approach to developing a system of continues automated monitoring of structural health is to use elastic waves excited in a given medium by a piezoelectric transducers network. Depending on their source and the geometry of the structure under con

Externí odkaz: https://doaj.org/article/81c66ca0c5354622ba36efb3c7e803ad

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