Výsledky vyhledávání - "Tavera Guerrero, Carlos"

Akademický článek

Blade oscillation mechanism for aerodynamic damping measurements at high reduced frequencies

Autor: Glodic Nenad, Tavera Guerrero Carlos, Gutierrez Salas Mauricio

Publikováno v: E3S Web of Conferences, Vol 345, p 03002 (2022)

Accurate prediction of aerodynamic damping is essential for flutter and forced response analysis of turbomachinery components. Reaching a high level of confidence in numerical simulations requires that the models have been validated against the exper

Externí odkaz: https://doaj.org/article/4b5fba9c61434f428fda0dd6b33ea8a7

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Steady-state aerodynamics tip gap influence in atransonic linear cascade at near stall

Autor: Tavera Guerrero, Carlos, Glodic, Nenad, Hans, Mårtensson

A comparison of steady-state aerodynamics for two tip gap configurations in the KTH transonic linear cascade is presented. The experimental campaign is performed for 1% and 2% tip clearances. The operational point is representative of an open-source

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______260::bcfc9a0db999bb33f145de652c466a3d
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-329255

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Validation of unsteady aerodynamics in a transonic linear cascade at first flex modeshape at near stall conditions

Autor: Tavera Guerrero, Carlos, Glodic, Nenad, Gutierrez, Mauricio, Mårtenson, Hans

Experimental and numerical, are presented in the transonic linear cascade (TLC) at KTH. Numerical results are recovered by SST turbulence model with a reattachment modification (RM) from commercial software Ansys CFX. This paper aims to compare the c

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=od_______260::6f00da9ad485b333297c1363e28d05c3
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-329245

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