Performance Assessment Limits in Transonic 3D Turbine Stage Blade Rows Using a Mixing-Plane Approach

AuthID
 P-003-2GT
3
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Tipo de Documento
Article
Year published
2010
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in JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, ISSN: 1738-494X
Volume: 24, Número: 10, Páginas: 2035-2042 (8)
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SCOPUS: 2-s2.0-78649715073
Wos: WOS:000282841100011
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ISSN: 1738-494X
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