Development of a method for geometrical modeling of the airfoil profile of an axial turbomachine blade-Reference-Cited by-同舟云学术

Development of a method for geometrical modeling of the airfoil profile of an axial turbomachine blade

Published:2019-10-16 Issue:1 (101) Volume:5 Page:29-38
ISSN:1729-4061
Container-title:Eastern-European Journal of Enterprise Technologies
language:
Short-container-title:EEJET

Author:

Borisenko Valeriy^ORCID,Ustenko Serhiy^ORCID,Ustenko Iryna^ORCID,Kuzma Kateryna^ORCID

Publisher

Private Company Technology Center

Subject

Applied Mathematics,Electrical and Electronic Engineering,Management of Technology and Innovation,Industrial and Manufacturing Engineering,Computer Science Applications,Mechanical Engineering,Energy Engineering and Power Technology,Control and Systems Engineering

Reference24 articles.

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2. Chislennoe issledovanie vliyaniya formy peredney kromki na effektivnost' turbinnoy reshetki;Homylev;Vestnik Nats. tehn. un-ta "KhPI": sb. nauch. tr. Temat. vyp.: Energeticheskie i teplotehnicheskie protsessy i oborudovanie,2011

3. Calculating axisymmetric gas flow trough vane row of turbine stage of non-traditional design;Mamaev;Problemy energetiki,2006

4. Vliyanie geometricheskih harakteristik turbinnoy stupeni na radial'niy gradient reaktivnosti;Levina;Teploenergetika,1996

5. Aerodynamic optimization of turbomachinery blades using evolutionary methods and ANN-based surrogate models;Mengistu;Optim Eng

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