Wszystkie pola: Wronkowicz, A. - Katalog OPAC zbiorów

Skocz do pozycji: 1.

Tytuł:: A Brief Review on NDT&E Methods For Structural Aircraft Components
Autorzy:: Wronkowicz-Katunin, A.
Powiązania:: https://bibliotekanauki.pl/articles/97992.pdf
Data publikacji:: 2018
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: NDT&E methods
non-destructive testing
non-destructive evaluation
aircraft structures
composite structures
Opis:: The paper presents a summary of non-destructive testing and evaluation (NDT&E) methods applied in inspections of structural aircraft components. This brief review covers the most commonly applied methods such as visual and penetrant inspections, tap-testing, eddy current inspections, shearography, thermography, acoustic emission testing, radiographic and tomographic inspections, and ultrasonic inspections. The general operating principles of these methods as well as their main advantages, limitations and application areas are described below.
Źródło:: Fatigue of Aircraft Structures; 2018, 10; 73-81
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

Skocz do pozycji: 2.

Tytuł:: Evaluation of Impact Damage in Composite Structures Using Ultrasonic Testing
Autorzy:: Wronkowicz-Katunin, A.
Dragan, K.
Powiązania:: https://bibliotekanauki.pl/articles/97897.pdf
Data publikacji:: 2018
Wydawca:: Sieć Badawcza Łukasiewicz - Instytut Lotnictwa
Tematy:: impact damage
composite structures
non-destructive testing
ultrasonic testing
image analysis
Opis:: Barely visible impact damage is one of the problems commonly occurring in composite elements during an aircraft operation. The authors described the mechanisms of impact damage formation and propagation in composite structures. The paper presents a performed analysis of an influence of impact parameters on the resulting damage, i.e. its detectability by means of visual observation as well as its extent determined based on ultrasonic tests results. The tests were conducted on the CFRP specimens with a wide range of impact damage cases obtained with combinations of variable impact energy and shapes of impactors. Additionally, an algorithm based on image processing and image analysis methods is proposed for the purpose of the effective evaluation of the ultrasonic data obtained.
Źródło:: Fatigue of Aircraft Structures; 2018, 10; 82-92
2081-7738
2300-7591
Pojawia się w:: Fatigue of Aircraft Structures
Dostawca treści:: Biblioteka Nauki

Artykuł

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