Zobrazeno 1 - 6
of 6
pro vyhledávání: '"K. M. Argu¨elles Di´az"'
Publikováno v:
Volume 6: Turbomachinery, Parts A and B.
The main objective is the numerical study of the noise generation in a single stage axial flow blower. For the present work, just the discrete noise generation (tonal noise) is dealt with. A numerical methodology based on a generalization of Lighthil
Publikováno v:
Scopus-Elsevier
This work develops the numerical modeling of a monoplane axial jet fan with symmetric blades. The goal of the study is the simulation of the flow inside a rotor with elliptic airfoils, where the Kutta condition cannot be satisfied. The unsteady 3D mo
Unsteady Rotor-Stator Interaction in an Axial Flow Blower: Part II — Deterministic Stresses Analysis
Publikováno v:
Volume 1: Symposia, Parts A and B.
Since the instantaneous phase-averaged flow field has been characterized and properly described through both numerical and experimental studies in a single stage axial flow blower, the next step is to identify the sources of unsteadiness related to b
Publikováno v:
Volume 2: Fora.
This work deals with a numerical simulation developed to predict the characteristic cooling times of a low-thermal diffusivity fuel-oil confined in the tanks of a wrecked ship. A typical scenario has been introduced, through the definition of tanks g
Publikováno v:
Scopus-Elsevier
In the usual operation of turbomachinery, some unsteady flow phenomena appear due to the non uniformity of the flow inside the rotor, when observed in the fixed reference frame. These phenomena are often related to the unsteady character of the press
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6de7efd3bbe9b8a755db926a6d6f7fdd
http://www.scopus.com/inward/record.url?eid=2-s2.0-0346903449&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-0346903449&partnerID=MN8TOARS
Publikováno v:
Scopus-Elsevier
The potential effect of the inlet guide vanes blockage is predominant in an axial one-stage configuration when the upstream flow field is considered. In the same way, rotor downstream, the main unsteadiness is provoked by the rotor wakes mixing-out a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f04b7105c2ce79ce4ca6981b36547533
http://www.scopus.com/inward/record.url?eid=2-s2.0-33847019979&partnerID=MN8TOARS
http://www.scopus.com/inward/record.url?eid=2-s2.0-33847019979&partnerID=MN8TOARS