Xiaosheng Zhang

Air Force Engineering University

Xi'an

China

SCHOLARLY PAPERS

1

DOWNLOADS

13

TOTAL CITATIONS

0

Scholarly Papers (1)

1.

High Cycle Fatigue Limit Assessment of Foreign Object Damaged Aerofoil Blades Considering the Residual Stress Induced by Impact

Number of pages: 46 Posted: 07 Oct 2024
Air Force Engineering University, Air Force Engineering University, Air Force Engineering University - Science and Technology on Plasma Dynamics Laboratory, Nanjing University of Aeronautics and Astronautics, Air Force Engineering University, affiliation not provided to SSRN, Air Force Engineering University, Air Force Engineering University and Nanjing University of Aeronautics and Astronautics
Downloads 13 (1,243,791)

Abstract:

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Fan blade, Foreign object damage, Residual Stress, High cycle fatigue, Critical distance