Zobrazeno 1 - 5
of 5
pro vyhledávání: '"J. D. Paduano"'
Publikováno v:
Journal of Turbomachinery. 121:517-524
This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were conducted at the NASA Lewis Research Center on a single-stag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bfce7e041152dbc991de11b001b60b0
https://doi.org/10.1115/1.2841346
https://doi.org/10.1115/1.2841346
Publikováno v:
Journal of Turbomachinery. 121:510-516
This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were conducted at the NASA Lewis Research Center on a single-stag
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e832983a3768be38f2671a5bcb74e164
https://doi.org/10.1115/1.2841345
https://doi.org/10.1115/1.2841345
Publikováno v:
Journal of Turbomachinery. 120:431-439
This paper describes the first experimental validation of transfer function modeling and active stabilization for axial compressors with circumferential inlet distortion. The inlet distortion experiments were carried out in a three-stage low-speed co
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9b1a301af3640ed2632ebf44f45d31c
https://doi.org/10.1115/1.2841734
https://doi.org/10.1115/1.2841734
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
Active stabilization of surge was implemented on an Allied Signal LTS-101 axi-centrifugal gas producer, reducing the surging mass flow by 1%, for an operating range increase of 11%. Control was achieved using high response sensors in the inlet and di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f0d071754788cc361b9a68d234459205
https://doi.org/10.1115/99-gt-438
https://doi.org/10.1115/99-gt-438
Publikováno v:
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery.
This paper presents an experimental and analytical investigation of compressor stability assessment during engine transient operation. A 2-dimensional, linear, compressible, state-space analysis of stall-inception (Feulner et al. (1996)) was modified
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d99a4d3c29edc1f589ad7ade2af91c02
https://doi.org/10.1115/99-gt-439
https://doi.org/10.1115/99-gt-439