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Scopus YÖKSİS DOI Eşleşti SJR Q1

Experimental investigation on Compression-After-Impact (CAI) response of aerospace grade thermoset composites under low-temperature conditions assisted with acoustic emission monitoring

Composite Structures · Ekim 2023

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YÖKSİS Kayıtları
Experimental investigation on Compression-After-Impact (CAI) response of aerospace grade thermoset composites under low-temperature conditions assisted with acoustic emission monitoring
Composite Structures · 2023 SCI-Expanded
Doç. Dr. HASAN ULUS →
YÖKSİS ISSN Eşleşmesi

Bu dergide (ISSN eşleşmesi) kurumun 12 kaydı bulundu.

YÖKSİS Kayıtları — ISSN Eşleşmesi
An experimental study on low velocity impact performance of bolted composite joints part 1: Influence of halloysite nanotubes on dynamic loading response
2021 ISSN: 0263-8223 SCI-Expanded Q1
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An experimental study on low velocity impact performance of bolted composite joints-part 2: Influence of long-term seawater aging
2021 ISSN: 0263-8223 SCI-Expanded Q1
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Experimental analysis of reinforced concrete shear deficient beams with circular web openings strengthened by CFRP composite
2020 ISSN: 0263-8223 SCI-Expanded
Doç. Dr. ŞAKİR YAZMAN →
The effects of stacking sequence on drilling machinability of filament wound hybrid composite pipes: Part-2 damage analysis and surface quality
2020 ISSN: 0263-8223 SCI-Expanded
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Experimental investigation of shear capacity and damage analysis of thinned end prefabricated concrete purlins strengthened by CFRP composite
2019 ISSN: 0263-8223 SCI-Expanded
Doç. Dr. ŞAKİR YAZMAN →
An experimental evaluation on the dynamic response of water aged composite/aluminium adhesive joints: Influence of electrospun nanofibers interleaving
2022 ISSN: 0263-8223 SCI-Expanded Q1
Doç. Dr. HASAN ULUS →
A Review on Drilling of FML Stacks with Conventional and Unconventional Processing Methods under Different Conditions
2022 ISSN: 0263-8223 SCI-Expanded Q1
Doç. Dr. ŞAKİR YAZMAN →
A Review on Drilling of FML Stacks with Conventional and Unconventional Processing Methods under Different Conditions
2022 ISSN: 0263-8223 SCI-Expanded Q1
Dr. Öğr. Üyesi MEHMET AKİF DOĞAN →
Effects of high pulling speeds on mechanical properties and morphology of pultruded GFRP composite flat laminates
2022 ISSN: 0263-8223 SCI-Expanded Q1
Doç. Dr. ŞAKİR YAZMAN →
Effect of oil pressure upon filament wound basalt/glass fibers hybrid polymer based composite pipes subjected to low velocity impact
2022 ISSN: 0263-8223 SCI-Expanded Q1
Doç. Dr. MEHMET TURAN DEMİRCİ →
Quasi-Static tensile loading performance of Bonded, Bolted, and hybrid Bonded-Bolted Carbon-to-Carbon composite Joints: Effect of recycled polystyrene nanofiber interleaving
2023 ISSN: 0263-8223 SCI-Expanded Q1
Doç. Dr. HASAN ULUS →
Experimental investigation on Compression-After-Impact (CAI) response of aerospace grade thermoset composites under low-temperature conditions assisted with acoustic emission monitoring
2023 ISSN: 0263-8223 SCI-Expanded Q1
Doç. Dr. HASAN ULUS →

Makale Bilgileri

Dergi Composite Structures
ISSN02638223
Yayın TarihiEkim 2023
Cilt / Sayfa321
DOI10.1016/j.compstruct.2023.117260
Scopus ID2-s2.0-85162171797
Özet Low-velocity impact (LVI) can provoke catastrophic failure depending on the impact energy, lay-up configuration, and the operating temperature in fiber-reinforced composite structures via damage accumulation during the service. Additionally, extreme operating temperature is an important factor affecting the damage initiation and growth mechanism and understanding the compression-after-impact (CAI) response is a promising way to predict the damage-growth dynamics. For this purpose, this study investigates the LVI response and CAI strength of composite laminates under the −55 °C temperature considering the low-temperature (LT) service conditions of aerospace applications. The experiments are performed on cross-ply ([0/90°]4s) and angle-ply ([±45°]4s) lay-up composites for impact energy levels of 1.4 J and 10 J. After LVI tests, the occurred damages are examined by infrared thermography (IRT). Furthermore, the effect of the impact damage on the failure mechanism under compression loading is elaborated using acoustic emission (AE) inspection. The CAI test results reveal that the LT increases the compressive residual strength. However, this change is directly related to the load and lay-up configuration. The alternation in the damage growth mechanism of angle-ply laminates under LT operating temperature is more significant compared to the cross-ply laminates.

Yazarlar (5)

1
Mahsa Seyyednourani
2
Sercan Akgun
3
Hasan Ulus
ORCID: 0000-0001-8591-8993
4
Mehmet Yildiz
ORCID: 0000-0003-1626-5858
5
Hatice S. Sas

Anahtar Kelimeler

Acoustic emission Compression test Environmental conditions Failure modes Impact behavior Infrared thermography Lay-up sequence

Kurumlar

Center for Composite Materials
Newark United States
Sabancı Üniversitesi
Tuzla Turkey
Scimago Dergi (ISSN Eşleşmesi)
Composite Structures
Q1
SJR Skoru1,660
H-Index226
YayıncıElsevier B.V.
ÜlkeNetherlands
Ceramics and Composites (Q1)
Civil and Structural Engineering (Q1)
Dergi sayfasına git

Metrikler

48
Atıf
5
Yazar
7
Anahtar Kelime

Sistemimizdeki Yazarlar

HU
HASAN ULUS
Doç. Dr.

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