Araştırma Makalesi

Comparative analysis of stress distributions and safety factor in tensile test specimens with different notch and hole geometries by finite element method

Cilt: 16 Sayı: 1 20 Şubat 2026
PDF İndir
EN

Comparative analysis of stress distributions and safety factor in tensile test specimens with different notch and hole geometries by finite element method

Abstract

This study analyzes the effects of different notch and hole geometries (V-Notched, U-Notched, circular hole) on stress concentration in Ti-6Al-4V (Grade 5) Titanium alloy tensile specimens to provide optimized design recommendations for aerospace and biomedical applications. Finite element method (ANSYS Workbench) was employed to analyze three geometries under 15000 N static tensile loading. SOLID186 20-node quadratic solid elements were used with optimal mesh (31100 elements) determined through convergence study. Von Mises stress distributions and stress concentration factors (Kt) were calculated and validated against Peterson and Neuber theoretical formulas with average error ±1.5%. Results revealed that V-Notched exhibited highest stress concentration (Kt = 5.78, σmax = 1156 MPa), while circular hole showed lowest (Kt = 2.25, σmax = 454.12 MPa). U-Notched demonstrated intermediate performance (Kt = 2.84, σmax = 995.45 MPa). Increasing notch root radius from 0.5 mm to 2.0 mm achieved 51% reduction in stress concentration factor. Maximum shear stress values were 232.74 MPa, 506.38 MPa, and 640 MPa for circular, U-Notched, and V-Notched respectively, while maximum normal stress values reached 467.06 MPa, 1015.1 MPa, and 1809 MPa. Safety factor analysis showed that circular hole configuration meets aerospace standards (FS = 2.05 > 1.5), while U-Notched (FS = 0.93) and V-Notched (FS = 0.80) fall below minimum safety criteria. U-Notched exhibited highest total displacement (1.210 mm), indicating compliance effects. For aerospace and biomedical applications, circular holes should be preferred over sharp notches (154% stress reduction), and minimum corner radius ≥2.0 mm is recommended. The critical finding that geometric optimization provides 2.6× safety improvement without material changes demonstrates the powerful role of design in structural reliability for weight-critical applications.

Keywords

Finite element method , Notched geometry , Safety factor , Stress analysis , Titanium alloy

Kaynakça

  1. ASTM B265-20. (2020). Standard specification for titanium and titanium alloy strip, sheet, and plate. ASTM International. https://doi.org/10.1520/B0265-20
  2. Azevedo, L., Kashaev, N., Horstmann, C., Ventzke, V., Furtado, C., Moreira, P. M. G. P., & Tavares, J. (2022). Fatigue behaviour of laser shock peened AISI D2 tool steel. International Journal of Fatigue, 165(107226). https://doi.org/10.1016/j.ijfatigue.2022.107226
  3. Boyer, R., Welsch, G., & Collings, E.W. (1994). Materials Properties Handbook: Titanium Alloys. ASM International
  4. Chmelko, V., Harakal’, M., Žlábek, P., Margetin, M., & Ďurka, R. (2022). Simulation of stress concentrations in notches. Metals, 12(1), 1–9. https://doi.org/10.3390/met12010043
  5. du Plessis, A., & Beretta, S. (2020). Killer notches: The effect of as-built surface roughness on fatigue failure in AlSi10Mg produced by laser powder bed fusion. Additive Manufacturing, 35 (101424). https://doi.org/10.1016/j.addma.2020.101424
  6. Dutt, A. K., Gwalani, B., Tungala, V., Carl, M., Mishra, R. S., Tamirisakandala, S. A., Young, M. L., Cho, K. C., & Brennan, E. B. (2019). A novel nano-particle strengthened titanium alloy with exceptional specific strength. Sci Reports, 9(11726). https://doi.org/10.1038/s41598-019-48139-8
  7. Fazlali, B., Upadhyay, S., Ashodia, S. A., Mesquita, F., Lomov, S. V., Carvelli, V., & Swolfs, Y. (2023). Specimen designs for accurate tensile testing of unidirectional composite laminates. Composites Part A, 175(107799). https://doi.org/10.1016/j.compositesa.2023.107799
  8. Haritos, G.K., Nicholas, T., Lanning, D.B. (1999). Notch size effects in HCF behavior of Ti-6Al-4V. International Journal of Fatigue, 21(7), 643-652. DOI: 10.1016/S0142-1123(99)00023-7
  9. Haseeb, S. A., Kumar, A. S., Chaitra, M. P., Vinaya, K. C., Gudal, S. S., Rahman, F. P., & Babaji, P. (2023). Finite element analysis to assess stress and deformation in bone with glass fiber reinforced poly ether ether ketone, zirconia, and titanium implants. Tzu Chi Medical Jornal, 35(3), 231-236. https://doi.org/10.4103/tcmj.tcmj_184_22
  10. Holmes, J., Sommacal, S., Das, R., Stachurski, Z., & Compston, P. (2023). Digital image and volume correlation for deformation and damage characterisation of fibre-reinforced composites: A review. Composites Structures, 315(116994). https://doi.org/10.1016/j.compstruct.2023.116994

Kaynak Göster

APA
Erdem Korkmaz, S., & Gavgalı, E. (2026). Comparative analysis of stress distributions and safety factor in tensile test specimens with different notch and hole geometries by finite element method. Gümüşhane Üniversitesi Fen Bilimleri Dergisi, 16(1), 160-178. https://doi.org/10.17714/gumusfenbil.1799320