Monday, 02. December 2024

Mo.5.A - Materials Characterisation

                 
Mo.5.A.1 Investigations on relationship between porosity and ultrasonic attenuation coefficient in CFRP laminates based on RMVM
S. Ding 1 , S. Jin 1 , Z. Luo 1 , H. Liu 1 , J. Chen 1 , L. Lin 1
1: Dalian University of Technology, Dalian, China
Manuscript
Mo.5.A.2 Impact Damage Detection in Graphene Doped CFRP Laminates
A. Güemes 1 , B. Larrañaga 1 , R. Moriche 2 , M. Sanchez 2
1: Universidad Politecnica de Madrid, Spain
2: URJC, Madrid, Spain
without Manuscript
Mo.5.A.3 Evaluation of CFRP-Reference Samples for Porosity made by Drilling and Comparison with Industrial Porosity Samples by Means of Quantitative X-ray Computed Tomography
B. Plank 1 , G. Rao 1 , J. Kastner 1
1: University of Applied Sciences Upper Austria, Wels, Austria
Manuscript
Mo.5.A.4 INSPECTION OF SICf/SIC CERAMIC MATRIX COMPOSITE SPECIMENS EMPLOYED FOR FATIGUE EXPERIMENTS VIA LABORATORY X-RAY COMPUTED MICROTOMOGRAPHY
Z. Quiney 1 , M. Bache 1 , J. Jones 1
1: Swansea University, UK
Manuscript
Mo.5.A.5 Short Time Evaluation of Metallic Materials’ Fatigue Potential Combining Destructive and Non-destructive Testing Methods
P. Starke 1 , H. Wu 1 , C. Boller 1
1: Universität des Saarlandes, Saarbrücken, Germany
Manuscript
Mo.5.A.6 Fault Detection in Aircraft Wiring using Enhanced Multi-pulse TDR Technique
M. Shirkoohi 1
1: London South Bank University, UK
Manuscript
Mo.5.A.7 Non-Destructive Evaluation of Aircraft Cables Using Ultrasonic Guided Wave Technique
A.Y.B. Chong 1 , S.-M. Tan 1 , R. Arondekar 1 , T. Parthipan 2 , P. Jackson 2 , S. Moustakidis 3 , V. Kappatos 1 , C. Selcuk 1 , T.-H. Gan 1
1: Brunel University, Cambridge, UK
2: Plant Integrity, Cambridge, UK
3: Centre for Research & Technology Hellas, Athens, Greece
Abstract with Powerpoint
Mo.5.A.8 On- and Off-line Ultrasonic Inspections to Characterize Components Build by SLM Additive Manufacturing
H. Rieder 1 , M. Spies 1 , J. Bamberg 2 , B. Henkel 2 , H.-U. Baron 2
1: Fraunhofer IZFP, Saarbrücken, Germany
2: MTU Aero Engines, München, Germany
Abstract with Powerpoint