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Maximizing multistage turbine efficiency by optimizing hub and shroud shapes and inlet and exit conditions of each blade row
| Naziv: | Maximizing multistage turbine efficiency by optimizing hub and shroud shapes and inlet and exit conditions of each blade row | Autori: | Petrović, Milan   ; Dulikravich, G.S.; Martin, T.J. |
Godina: | 2000 | Publikacija: | International Journal of Turbo and Jet Engines | ISSN: | 0334-0082 International Journal of Turbo and Jet-engines Pretraži identifikator |
Izdavač: | Walter de Gruyter GmbH | Tip rezultata: | Naučni članak | Kolacija: | vol. 17 br. 4 str. 267-278 | DOI: | 10.1515/TJJ.2000.17.4.267 | WoS-ID: | 000089616300003 | Scopus-ID: | 2-s2.0-0034339331 | URI: | https://machinery.mas.bg.ac.rs/handle/123456789/185 https://enauka.gov.rs/handle/123456789/572594 |
Projekat: | The authors are grateful for National Science Foundation Grant, DMI-9522854 and DMI-9700040 monitored by Dr. George Hazelrigg and for NASA Lewis Research Center Grant NAG3-1995 facilitated by Dr. John Lytle and supervised by Dr. Kestutis Civinskas. | M-kategorija: | 21M21 - Vodeći međunarodni časopis kategorije M21 |
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