Modified Three-Parameter Model to Predict Compressor Blade Fatigue Life under Vibration Loading-Reference-Cited by-同舟云学术

Modified Three-Parameter Model to Predict Compressor Blade Fatigue Life under Vibration Loading

Published:2019-07 Issue:4 Volume:32 Page:04019034
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Yakui¹,Guo Shuxiang²,Zhang Zhongping²,Shang Bolin³

Affiliation:

1. Graduate Student, Aeronautical and Astronautical Science and Technology, School of Air Force Engineering Univ., Xi’an 710038, Republic of China (corresponding author).

2. Professor, Aeronautical and Astronautical Science and Technology, School of Air Force Engineering Univ., Xi’an 710038, Republic of China.

3. Professor, Aeronautical and Astronautical Science and Technology, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, Republic of China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001009

Reference47 articles.

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2. Advanced Beam Formulations for Free-Vibration Analysis of Conventional and Joined Wings

3. A critical plane-strain energy density criterion for multiaxial low-cycle fatigue life under non-proportional loading

4. A study of the effects of cyclic thermal stresses on a ductile metal;Coffin L. F. J.;J. Eng. Mater. Technol.,1954

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