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《Analysis of Stress and Vibration of Blade for Aero Turbocharger》
LIN Hai-ying;CHEN Meng
2009, 29 (
6
): 44-49. DOI:
10.3969/j.issn.1006-1355.2009.06.044
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On the base of structure remodeling and aerodynamic designof micro turbocharger for aero piston engine, this paper described the stress and vibration analysis of blades for
turbocharger. The results shows that in the rotation range of the rotor, the blade of compressor and turbine will work safely.
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