04393ntm a2200373 i 4500 0 0 lcc 0 1 REF 10000 10000 2020-10-15 0 FTKA .T36 2019 r Thesis T000000960 2021-03-16 00:00:00 1 2020-10-15 THESIS 0 0 lcc 0 0 REF 10000 10000 2020-10-15 0 CD12707 T000000961 2021-12-06 00:00:00 1 2020-10-15 THESIS 0 0 lcc 0 1 REF 10000 10000 2021-03-16 0 FTKA .T36 2019 r Thesis 2021-03-16 00:00:00 2021-03-16 THESIS 94345 94351 MY-KuUP 20251125105735.0 t||||fr|||| 000 0 ta 201015t2 2 M a|||fram|| 000 0 eng d THE0008910(Local) hardback UMP eng UMP rda FTKA .T36 2019 r Thesis Tan, Sze Pei, author. Numerical study of crashworthiness on honeycomb filler subjected to impact loading / Tan Sze Pei Kuantan, Pahang : UMP, 2019 © 2019 xiii, 103 pages : illustrations (some color) ; 30 cm. + 1 CD-ROM text rdacontent text rdacontent unmediated rdamedia computer rdamedia volume rdacarrier computer disc rdacarrier text file PDF rda Faculty of Engineering Technology Thesis (Master of Science) -- Universiti Malaysia Pahang – 2019 Includes bibliographical references Honeycomb filler is known as a good filler for energy absorbing devices in car. Many types of research about honeycomb filler under axial impact had been done and proposed in the literature. However, when it comes to the real situation in an accident, a collision is not only coming from a frontal impact (axial loading). A collision might also come from a different angle (oblique loading). Therefore, crashworthiness in several impact angles are important concern in designing a safe vehicle. The crashworthiness criteria, namely energy absorption (EA) and specific energy absorption (SEA) are related to loading parameters. Safety is the main concern in designing an energy absorber. However, reducing the extra weight caused by the energy absorber is also one of the concerns for manufacturers. This is because the lighter the weight the vehicle has the lesser fuel is consumed to be eco-friendly. In this study, the main objective is to study the performance of honeycomb fillers by different cross-sectional design versus thickness subjected to different angles of impact loading. The investigation is carried out by Finite Element (FE) simulation using ABAQUS software. The investigations of all FE models are carried out by the dynamic impact test. Numerical investigation studies the reaction of three types of honeycomb filler geometric designs which are circular honeycomb filler, hexagon honeycomb filler and multicell. The diameter of every single cell for honeycomb filler is fixed at 10.4 mm. Three different thicknesses of every cell are investigated which are t = 0.06 mm, 0.12 mm, and 0.18 mm. All models are carried out by dynamic impact with both axial and oblique loading which 𝜃 = 0°, 10°, 20°, and 30°. The material assigned to all models is aluminium alloy AA6060-T4. According to simulation result in this study, hexagon honeycomb filler is the best structural design. The result of EA, SEA, and CFE of hexagon honeycomb filler is 120 % higher than circular honeycomb filler and 230 % higher than multicell filler. The crashworthiness is influenced by the thickness of honeycomb filler, the thickness of honeycomb filler increased, then crashworthiness criteria performance increased. When thickness increased from 0.06 mm to 0.12 mm, the EA and CFE increased by approximately 290 % and SEA increased by approximately 150 %. When thickness increased from 0.12 mm to 0.18 mm, the EA, SEA, and CFE increased by approximately 170 %, 120 % and 190 %, respectively. When thickness increased from 0.06 mm to 0.18 mm, the EA, SEA, and CFE increased by approximately 500 %, 170 %, and 550 %, respectively. The increment is much higher than the aspect ratio of thickness of 200 %, 150 %, and 300 % respect to 0.06 mm to 0.12 mm, 0.12 mm to 0.18 mm, and 0.06 mm to 0.18 mm. Lastly, the axial loading and oblique loading of honeycomb fillers with angles, 𝜃 = 0° - 30° are studied. Results showed that the performance of EA and SEA decreased when angles, 𝜃 increased. In conclusion, the overall result showed that hexagon honeycomb filler is the best model in terms of geometry, thickness, and angle of loading. Faculty of Engineering Technology Dissertations Universities and colleges Dissertations Theses lcc THESIS