Determination of impeller blade fillet radius for productive finish milling
Author:
Funder
Ministerstvo Průmyslu a Obchodu
Publisher
Springer Science and Business Media LLC
Subject
Industrial and Manufacturing Engineering,Computer Science Applications,Mechanical Engineering,Software,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00170-023-11483-1.pdf
Reference24 articles.
1. Rahtore AS, Ravichandrakumar KB (2017) Parametric study on impeller exit blade width variation on centrifugal compressor performance. Int J Aeros Mech Eng 4. ISSN(O): 2393–8609
2. Li C, Wang J, Guo Z, Song L, Li J (2019) Aero-mechanical multidisciplinary optimization of a high speed centrifugal impeller. Aeros Sci Technol 95:105452. https://doi.org/10.1016/j.ast.2019.105452
3. Wu T, Shao L, Wei X, Ma X, Zhang G (2019) Design and structure optimization of small-scale radial inflow turbine for organic Rankine cycle system. Energy Convers Manage 199:111940. https://doi.org/10.1016/j.enconman.2019.111940
4. Moussavi SA, HajilouyBenisi AH, Durali M (2017) Effect of splitter leading edge location on performance of an automotive turbocharger compressor. Energy 123:511–520. https://doi.org/10.1016/j.energy.2017.02.011
5. Omidi M, Liu Y, Mohtaram S, Li S (2022) Investigating on performance parameters and flow field of centrifugal compressor based on the splitter blade leading edge’s location effect. J Mech Sci Technol 36(8):4015–4020. https://doi.org/10.1007/s12206-022-0722-5
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