Fatigue Damage–Based Topology Optimization of Helicopter Tail Rotor Pitch Arm-Reference-Cited by-同舟云学术

Fatigue Damage–Based Topology Optimization of Helicopter Tail Rotor Pitch Arm

Published:2022-09 Issue:5 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Demir Süleyman¹^ORCID,Kurt Mustafa²,Kotil Temel³

Affiliation:

1. Ph.D. Student, Institute of Science and Technology, Marmara Univ., Göztepe Campus, Institutes Bldg. Floor: 2 Kadıköy, Istanbul 34722, Turkey (corresponding author). ORCID: .

2. Professor, Dept. of Mechanical Engineering, Marmara Univ., Campus Kadıköy, Istanbul 34722, Turkey.

3. Professor, Dept. of Mechatronic Engineering, Istanbul Commerce Univ., Ornektepe, Imrahor 88/2 Beyoglu, Istanbul 34445, Turkey.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001471

Reference37 articles.

1. Bannantine, J. A., J. J. Comer, and J. L. Handrock. 1990. Fundamentals of metal fatigue analysis. Englewood Cliffs, NJ: Prentice Hall.

2. Optimization of Structural Topology, Shape, and Material

3. Topology Optimization

4. Bishop, N. W. M., and F. Sherratt. 2000. Finite element based fatigue calculations. Hamilton, UK: NAFEMS.

5. A mixed FEM approach to stress-constrained topology optimization

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