Zobrazeno 1 - 10
of 24
pro vyhledávání: '"Zhi-tao Mu"'
Publikováno v:
Advanced Materials Research. :31-34
Using the virtual crack closure technique (VCCT), an interface element that can calculate stress intensity factors (SIFs) directly and simulate the crack propagation conveniently has been developed. Based on an accelerated corrosion experiment, the f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7f0b9e400e90fa2c2716148efb7c7154
https://doi.org/10.4028/www.scientific.net/amr.998-999.31
https://doi.org/10.4028/www.scientific.net/amr.998-999.31
Publikováno v:
Advanced Materials Research. :59-62
With the aid of scanning electron microscope and energy spectrum analysis, the present thesis made a research on the fatigue fracture surface of AA 6A02 with corrosion damage as well as the effect of alloy element Si, Mg and the corrosion damage on t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b960d63c31055b5e8bb72d32465f609
https://doi.org/10.4028/www.scientific.net/amr.998-999.59
https://doi.org/10.4028/www.scientific.net/amr.998-999.59
Publikováno v:
Advanced Materials Research. 937:150-153
Experimental investigations of fatigue cracking behavior of LC9 aluminum alloy (AA LC9) subjected to elevated temperature were conducted with scanning electron microscope (SEM). Results indicate elevated temperature is important for the fatigue crack
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9153602774761d41aefa13878b0baac3
https://doi.org/10.4028/www.scientific.net/amr.937.150
https://doi.org/10.4028/www.scientific.net/amr.937.150
Publikováno v:
Applied Mechanics and Materials. :66-69
This paper investigates the growth behavior of fatigue cracks initiated at corrosion pits in laboratory coupons of LC9 aluminum alloy subjected to a transport aircraft loading spectrum. Corrosion pits were introduced by exposing the coupons to EXCO s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::54ac2844fa8a313a0f44450d0e0c9db2
https://doi.org/10.4028/www.scientific.net/amm.488-489.66
https://doi.org/10.4028/www.scientific.net/amm.488-489.66
Publikováno v:
Advanced Materials Research. 842:374-377
Considering the degradation effect of corrosion damage on fatigue behavior of aero aluminum alloy, the present thesis made a research on corrosion fatigue crack growth rate. Taking into account the effect of load frequency on fatigue crack growth, a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::176cf3b431eef5d01a18595b594207da
https://doi.org/10.4028/www.scientific.net/amr.842.374
https://doi.org/10.4028/www.scientific.net/amr.842.374
Publikováno v:
Applied Mechanics and Materials. :348-351
Three different analysis methods was put forward to carried out aircraft aluminum alloy structure corrosion damage forecasting,and comparison analysis of different method which included basic forecasting caculation principle and forecasting accuracy
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::43eafdfcd324bac2d6b7187dac4a8b0a
https://doi.org/10.4028/www.scientific.net/amm.268-270.348
https://doi.org/10.4028/www.scientific.net/amm.268-270.348
Publikováno v:
Proceedings of the 2015 2nd International Conference on Machinery, Materials Engineering, Chemical Engineering and Biotechnology.
Based on the theory of finite rotation beam, together with the finite element method, the rotor dynamic model is established, and the relationship of strain and displacement in the strain energy of blade is solved by introducing the generalized Danie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc595f9b394cc224dc27544ea34e3fa3
https://doi.org/10.2991/mmeceb-15.2016.146
https://doi.org/10.2991/mmeceb-15.2016.146
Publikováno v:
Proceedings of the 2015 2nd International Conference on Machinery, Materials Engineering, Chemical Engineering and Biotechnology.
The deformation of blades effected by gust would endanger the safety of wind turbine. Based on blades elastic deformation theory ,We established a model of blades rotation transient response ,studied the characteristics of blades transient response e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e55ef6e4e34d438c9bb1d933b00c88f1
https://doi.org/10.2991/mmeceb-15.2016.192
https://doi.org/10.2991/mmeceb-15.2016.192
Publikováno v:
Proceedings of the 2016 5th International Conference on Advanced Materials and Computer Science.
In order to investigate the corrosion damage of aviation steel material in the atmospheric environment, the present study used the 30CrMnSiA steel specimen to carry out the accelerated corrosion test simulated aviation steel material under the airpor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3dd44454a30e828a06b7467af6df1743
https://doi.org/10.2991/icamcs-16.2016.191
https://doi.org/10.2991/icamcs-16.2016.191
Publikováno v:
Key Engineering Materials. :81-84
Corrosion fatigue is a form of degradation subjected to combined damage of mechanical stress and corrosive medium, which is an issue in aircraft industry. Experimental investigations on prior corrosion fatigue cracking behavior of LY12CZ were conduct
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2eb06b8181356a60515a32ca94054816
https://doi.org/10.4028/www.scientific.net/kem.525-526.81
https://doi.org/10.4028/www.scientific.net/kem.525-526.81