Numerical simulation and experiments of titanium alloy engine blades based on laser shock processing-Reference-Cited by-同舟云学术

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Numerical simulation and experiments of titanium alloy engine blades based on laser shock processing

Published:2015-01 Issue: Volume:40 Page:164-170
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Pengyang,Huang Shikun,Xu Haifeng,Li Yuxi,Hou Xiaoli,Wang Quandai,Fu Weiping,Fang Yingwu

Funder

Shaanxi Provincial Natural Science Foundation of China

State Key Laboratory of Mechanical Transmission Open Foundation of China

National Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Analytical stress analysis of annular FGM sandwich plates with non-uniform shear and normal tractions, employing a zigzag-elasticity plate theory;Alipour;Aerosp. Sci. Technol.,2014

2. Simulation-based optimization of laser shock peening process for improved bending fatigue life of Ti–6Al–2Sn–4Zr–2Mo alloy;Bhamare;Surf. Coat. Technol.,2013

3. Thermomechanical bending response of FGM thick plates resting on Winkler–Pasternak elastic foundations;Bouderba;Steel Compos. Struct.,2013

4. Effect of initial surface topography on the surface status of LY2 aluminum alloy treated by laser shock processing;Dai;Vacuum,2012

5. Nonlinear axisymmetric response of FGM shallow spherical shells on elastic foundations under uniform external pressure and temperature;Duc;Eur. J. Mech. A, Solids,2014

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2. Spatial-temporal characteristics analysis of laser-induced shockwave pressure by reverse optimization with multi-island genetic algorithm;Journal of Laser Applications;2024-07-19

3. Finite-element simulation of residual stresses induced by laser shock peening in TC4 samples structurally similar to a turbine blade;Frattura ed Integrità Strutturale;2023-12-17

4. Theoretical and experimental harmonic analysis of cracked blade vibration;Measurement;2023-11

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