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Effect of an Axially Tilted Variable Stator Vane Platform on Penny Cavity and Main Flow
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In
Journal of turbomachinery 144(2), Seiten/Artikel-Nr.:021010
2022 & 2021
Published Online: September 29, 2021
Online
DOI: 10.1115/1.4052314
Einrichtungen
- Lehrstuhl und Institut für Strahlantriebe und Turboarbeitsmaschinen (413510)
- Lehrstuhl und Institut für Strahlantriebe und Turbomaschinen (413510)
Thematische Einordnung (Klassifikation)
DDC: 600
Dokumenttyp
Journal Article
Format
online
Sprache
English
Anmerkung
Peer reviewed article
Externe Identnummern
SCOPUS: SCOPUS:2-s2.0-85127387760
WOS Core Collection: WOS:000735286000004
OpenAlex: W4256031035
Interne Identnummern
RWTH-2021-09097
Datensatz-ID: 828356
Beteiligte Länder
Germany
Related:
Contribution to a book/Contribution to a conference proceedings
Effect of an Axially Tilted Variable Stator Vane Platform on Penny Cavity and Main Flow
Proceedings of ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition : June 7-11, 2021, virtual, online / conference sponsor: International Gas Turbine Institute. - Volume 2: Turbomachinery. - Axial flow fan and compressor aerodynamics
ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition, onlineonline, 7 Jun 2021 - 11 Jun 2021
New York, N.Y. : The American Society of Mechanical Engineers GT2021-59182, V02AT31A027; 12 Seiten (2021) [10.1115/GT2021-59182]
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RIS
; Clarivate Analytics Master Journal List ; Current Contents - Engineering, Computing and Technology ; Essential Science Indicators ; IF < 5 ; IF < 5 ; JCR ; PubMed Central ; SCOPUS ; Science Citation Index Expanded ; Web of Science Core Collection
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